Title 
Author(s) 


Smart Structures in Aerospace Technology 
Santini, P 


ICASVONKARMANLECTURE


Working Together  International Aero Engines' V2500 Program 
Eccleston, B., Cheffins, J., Wolfe, B 


General lectures


AEREA  A European Research Initiative 
Kroll, W 
Advanced OnBoard Computing and Data Processing: A Primary Condition for the Functionality of Modern High Performance Aircraft 
Scheidt, H., Rapp, H 
Innovative Aspects of the Boeing 777 Development Program 
Breuhaus, R.S., Fowler, K.R., Zanatta, J.J 




CFD DEVELOPMENT I


A Cartesian Cut Cell Method for Unsteady Flows Involving Freely Moving Bodies 
Yang, G., Causon, D.M., Ingram, D.M., Saunders, R 
Numerical Investigation of Strongly NonLinear Transonic Flow Problems around the Airfoil 
Yamamoto, S 
Solution of the NavierStokes Equations for the Flow around an Aerofoil in an Oscillating Free Stream 
Shaw, S., Qin, N 
Special Issues in Unsteady NavierStokes Simulations with Deforming Bodies 
Hoffren, J 


FLUID PHYSICS I


Challenges and Opportunities in Fluid Mechanics Research 
Hefner, J.N., Sellers III, W.L., Thomas, J.L., Wlezien, R.W., Antcliff, R.R 
Study for Reynolds Number Effect on CimM of 2Dimensional Airfoils 
Yoshida, K., Ogoshi, H 
Experimental Study on Transonic Shock Wave/Turbulent Boundary Layer Interactions and Separation Instabilities. Suction and Reynolds Number Effects 
Caruana, D., Bulgubure, C., Mignosi, A 
A Review of Research at DRA on Active and Passive Control of Shock Waves 
Ashill, P.R., Fulker, J.L., Simmons, M.J., Gaudet, I.M 
On Sound Transmission through Boundary Layers of Aircraft Fuselages and Engine Ducts 
Campos, L.M.B.C., Oliveira, J.M.G.S., Serrao, P.G.T.A, Kobayashi, M.H 


FLIGHT AT HIGH ANGLE OF ATTACK I


The Study of WingRock Characteristics on Slender Delta Wings at High AOA 
Hsiao, F.B., Yang, J.S 
Flow Analysis and Control Surface Evaluation at High Angles of Attack for Enhanced Manoeuvrability 
Tristrant, D., Renier, O., Farcy, D 
Controlling Aerodynamic Hysteresis Loop of Wing during Pitching Oscillation by Spanwise Blowing 
Qin, Y.H., Zhuang, F.G., Shen, L.M 
Flight Dynamics of a Vectored Thrust Aircraft 
Granasy, P 


ENVIRONMENTAL ISSUES


Determinants of Emission from Ground Operations of Aircraft 
Caves, R.E., Jenkinson, L.R., Brooke, A.S 
Methods to Assess Aircraft Engine Emissions in Flight 
Deidewig, F., Dopelheuer, A., Lecht, M 
Soot Emissions from Jet Aircaft 
Lilenfeld, H.V., Whitefield, P.D., Hagen, D.E 
NASA Noise Reduction Programs for Advanced Transport Aircraft 
Stephens, D.G., Powell, C.A., Cazier, Jr., F.W 
Civil Aircraft and Their Noise Impact on the Environment of the AthensSpata Airport 
Yiparakis, N.J., Lambrianidis, G 


STRUCTURAL DESIGN I


Optimisation of Highly Loaded Joints 
Rispler, A.R., Steven, G.P 
Structure Design Concepts for the Next Generation Supersonic Transport 
Ermanni, P., Braidley, I., Rib6re, B 
Bird Impact Resistance of Small Transport Aircraft 
Bedrich, L., Mertl, V 
Development of a Structural RPV Section Serving as an Integral Fuel Tank made of Sandwich CFRP 
Gali, S., Ghilhai, G., Peled, D., David, A., Sela, N., Derwish, Y 


PILOT ASSISTANCE


A Generic Architecture for InFlight Crew Assistant Systems Based on Advanced Information Processing Technology 
Zuidgeest, R.G., Urlings, P.J.M 
A New Design Approach for a Pilot Advisory System in AirtoAir Interceptions 
Yaakov, Y., Shinar, J., Wolfshtein, M., Boneh, A 
An AI Situational Pilot Model for RealTime Applications 
Burdun, I.Y 
The Cost Effective HeadUp Display in Trainer Aircraft 
Spring, H., Inabnit, M 


AERODYNAMICS I (Student Session)


Modelling and Identification of NonLinear Unsteady Aerodynamic Loads by Neural Networks and Genetic Algorithms 
Marques, F., Anderson, J 
Simulation of Unsteady Aerodynamic Effects of Isolated Vortices Close to the Airfoil 
Mitrovic, C 
Numerical Simulations of Large Eddies in the Compressible MixingLayer 
Ramella, F 
Wall Turbulence Manipulation by Outer Layer Devices 
ReisoliMatthieu, F 


UNSTEADY AERODYNAMICS I


Helicopter Rotor Downwash Calculation using the Vortex Element Method for the Wake Modelling 
Papanikas, D.G., Spyropoulos, A.J., Fertis, D.K., Margaris, D.P 
Application of an Unsteady TwoEquation Turbulence Model to the Numerical Prediction of the Transonic Buffet of an Airfoil 
Arina, R., Ceresola, N., Piantä, P.G 
Cyclic Acceleration Technique for Solving Unsteady Transonic Small Perturbation Equations 
Wayan Tjatra, I., Wandana, I 


AEROSPACE FLIGHT DYNAMICS


NonEquilibrium Reentry 
Filatyev, A.S., Yanova, O.V 
Chattering Arc in ThreeDimensional Flight 
Chern, J.S., Chen, Y.H., Hong, Z.C 
Aerodynamic Stabilization System for Small Satellites 
Sarychev, V.A., Camelier, I.A., Paglione, P 
Theoretical and Experimental Determination of Flight Performances of an Airplane in Martian Atmospheric Flight 
Teofilatto, P 


FLIGHT CONTROL I


Flight Safety Aspects with Modern Flight Control Systems 
Chatrenet, D 
FlyByWire for the Saab 2000  Concept, Development and Testing 
Singer, G., Persson, U 
Application of the Fuzzy Logic Control Theory to the Design of Aircraft Flight Control Systems 
Zhou, Z.Q., Reichert, G 
Method for Determining the Force Characteristics of a Nozzle under the Exposure to External Supersonic Flow 
Lokotko, A.V 


UNMANNED AIR VEHICLES


High Altitude Long Endurance (HALE) UAV for Intelligence Missions 
Tsach, S., Yaniv, A., Avni, H., Penn, D 
Development Approach of the HERON Medium Altitude Long Endurance UAV 
Vitali, J., Tsach, S., Avni, H., Gali, S., Weissberg, V 
Designing Process of Unmanned Aerial Vehicles 
JaxaMalachowski, R 


FINITE ELEMENT MODELLING


The Use of Genetic Algorithms in Dynamic FiniteElement Model Identification for Aerospace Structures 
Dunn, S.A 
Nonlinear Finite Element Analysis of Fluttering Plate in Transonic Unsteady Potential Flows 
Wayan Tjatra, I., Kurniawan, R 
Use of Artificial Neural Network for the Evaluation of SEA Coupling Loss Factor and AHL Damping Parameters 
Sorrentino, A., Vitiello, P., Romano, G., Dovstam, K 


FLOW INTERACTIONS


Rear Fuselage Flow Characteristics for a Complete WingBody Configuration at Transonic Conditions 
Coustols, E., S6raudie, A., Mignosi, A 
Theoretical and Experimental Studies of Vectoring Jets Effects on UnderWing Stores and their Release Trajectories 
Nangia, R.K., Ross, J.A., Peto, J.W 
Aerodynamic Assessment of Lateral Jet Sheets and Their Influence on WingBody Combinations for Some Blowing Arrangements 
Neamtu, M 
Canard Influence on the Boundary Layer of a Forward Swept Wing 
Lombardi, G., Morelli, M., Waller, D 
Mean Characteristics of Flow in Junctures of Swept Wings and Bodies 
Khan, M.J., Ahmed, A 


BOUNDARY LAYER STABILITY AND TRANSITION


A Linear Stability Analyser Suitable for Integration in Wing Performance Calculation Procedures 
Masson, C., Langlois, M., Paraschivoiu, I 
Numerical Investigation of the Effects of Sweep Angle on the BoundaryLayer Transition in High Speed Flight 
Shahpar, S 
Transition Control on a Transonic Laminar Airfoil with Suction Panel 
Jorgensen, L., Nitsche, W 
Hybrid Laminar Flow Nacelle Design 
Lecordix, J.L., Muhender, A., Lecossais, E., Godard, J.L., Hepperle, M 
A New Reconfiguration Concept for Flight Control Systems in Case of Actuator and Control Surface Failures 
Baumgarten, C, Heine, W 


FLIGHT DYNAMICS AND CONTROL


On Some Analytical Studies of Unsteady and NonLinear Longitudinal Stability 
Campos, L.M.B.C., Azinheira, J.R.C., Fonseca, A.A 
Integrated T&E Approach to Store Separation  Dim Past, Exciting Future 
Cenko, A., Richardson, P., Talbot, M., Loezos, S., Chaddock, D., Piranian, A 
Gust Alleviation Analysis for Flexible WingTail Configurations 
Gennaretti, M., De Troia, R., Tancredi, G., Morino, L 
Feasibility of Gravity Gradient Technology for Fighter Aircraft 
Blaylock, J.G., Swihart, D.E., Barfield, A.F 
On the Development of Flexible Aircraft Equations of Motion 
Ro, K.S., Barlow, J.B 
Dihedral Effect for Straight Tapered and Twisted Wings 
Gili, P 
Optimal Midcourse Trajectories for Precision Guided Munitions with Collocation and Nonlinear Programming 
Tekinalp, O., Arslan, E.M 


ROTORCRAFT


Conceptual Design and Proposed Development of the GAP4 MultiPurpose Small Utility Helicopter 
Schräge, D.P., Yillikci, Y.K., Phillips, J.W., Mavris, D.N 
Hover Performance of a Rotor with Deployable Flaps 
Nagabhushan, B.L., Shaban, A.I. 
The Development of a Knowledge Based System to Aid Helicopter Rotor Blade Design 
Hamilton, J.R., Clarkson, P.J., Burgess, S.C., Newland, D.E 
Wind Tunnel Testing of a 1 /3rd Scale Model Gyroplane 
Coton, F.N., Smrcek, L, Pätek, Z 
Feasibility Study and Mission Requirement for HSCT 
Mizuno, H., Hagiwara, S 


STRUCTURAL DESIGN II


SpecialPurpose Programs for Structural Design and Optimization 
Rothwell, A., Heerschap, M.E 
Analysis of Measured InFlight Tail Loads 
Gelder, P.A. van 
Theoretical Assessment, Numerical Simulation and Comparison with Tests of Birdstrike on Deformable Structures 
Anghileri, M., Sala, G 
Strength Estimation Method for Undamaged, Damaged and Repaired Honeycomb Structures 
Urinovsky, V., Coldbeck, D.P., Smrcek, L 


RELIABILITY AND MAINTAINABILITY


Heavy Transport Aircraft Reliability Study 
Chiesa, S., Gianotti, P., Maggiore, P 
GMADS  Groundbased Maintenance Aid and Diagnostic System 
Stenmarck, J 
Turbojet Engine Diagnostic System based on Compressor Blade Vibration and Vibroacoustic Analysis 
Dabrowski, H., Kudelski, R., Spychala, J., Szczepanik, R., Szczepankowski, A., Witos, M 
Extension in Calendar Life Limit for Aircraft Structure 
Ahmad, M., Ghafoor, A 


AERODYNAMICS II (Student Session)


Application of an Improved Integral Turbulent Boundary Layer Model with Moderate Separation Correction on NACA Series and Low Speed Supercritical Airfoil Derivatives 
Kostic, I 
An Inverse Method for the Design of Airfoils 
Nagaoka, T., Morishita, E 
Theoretical Study of a Mission Adaptive Wing 
Martins, A.L., Catalano, F.M 
Using the Fluent Program for Optimisation of the Fowler Flap System for the UltraLight Aeroplane 
Strnad, B.R 


CFD DEVELOPMENT II


Progress in the Development of Computational Aerodynamic Design Methods: Inverse Procedures 
Malone, J.B 
Turbulent Flow Calculations for Complex Aircraft Geometries using Prismatic Grid Regions in the SAUNA CFD Code 
Peace, A.J., Chappell, J.A., Shaw, J.A 
Numerical Methods for Simulating the Flow over an Airfoil Covered with a Thin Layer of Liquid 
Boelens, O.J., Moeleker, P.J.J., Jong, H. de, Hoeijmakers, H.W.M. 
Inverse Wing Design and Optimization using the Euler Flow Equations 
Sedin, Y.C.J., Larsson, T 
Vortical Flow Simulation using an UnstructuredGrid Euler Method 
Raj, P., Kinard, T.A., Vermeersch, S.A 


WIND TUNNEL ANALYSIS AND INSTRUMENTATION


An Experimental Investigation into the Rationale of the Application of Wind Tunnel Wall Corrections 
Ashill, P.R., Goodyer, M.J., Lewis, M.C 
Numerical Simulation of Flowfields of the NAL TwoDimensional Transonic Wind Tunnel 
Matsuno, K., Satofuka, N., Sudani, N., Fukuda, M., 
Optimization of the Performance of Internal SixComponent StrainGage Windtunnel Balances with FEM 
Zhai, J.N., Ewald, B., Hufnagel, K 
Generalization of Data Reduction Routines for Model Attitude, Force and Moment Measurements in the Wind Tunnels of the Aeronautical Institute Zarkovo 
Vukovic, Dj 
Complete Analytical Model to Describe the TestLeg of Scirocco PWT 
De Filippis, F., Schettino, A., Serpico, M., Borrelli, S 


DESIGN AND DEVELOPMENT


The Effective Management of Aerospace Projects through Process Modelling 
Balthazor, L.R 
A Virtual Rafale 
Pechaud, J., Rouchon, C 
An AngloUS View of Aircraft Design Education 
Whitford, R 
System Synthesis in Preliminary Aircraft Design using Statistical Methods 
DeLaurentis, D., Mavris, D.N., Schräge, D.P 
HighCapacity Subsonic Transport Projects 
Fielding, J.P 
On the Subsonic/Supersonic, Yawed Sinusoidal Gust over an Airfoil 
Soviero, P.A.O., Resende, H.B 


SUPERSONIC TRANSPORT AIRCRAFT


European 2nd Generation Supersonic Commercial Transport Aircraft 
Green, P.K., Pacull, M., Reimers, H.D 
The Oblique Flying Wing as the New Large Aircraft 
Li, P., Seebass, R., Sobieczky, H 
Aerodynamic Optimization of Supersonic Transport Configurations 
Orlowski, M., Hermann, U 
Flap Systems on Supersonic Transport Aircraft 
Nicholls, K.P 
The Long Term Elevated Temperature Behaviour of Materials: A Key Issue.for the Next SST 
Barbaux, Y.P., GuedraDesgeorges, D., Cinquin, J., Fournier, P., Lapasset, G 


DESIGN AND ANALYSIS OF COMPOSITES


The Development of a Composite Root Attachment Lug 
Cathro, R.C., Reid, R.G., Huston, R.J 
Textile Routes to Damage Tolerant Composite Structures for Aerospace Applications 
Backhouse, R., Bibo, G.A., Hogg, P.J., Mills, A 
Compressive Behaviour of Composite Panels Containing ImpactInduced Damages and Holes: Experimental and Numerical Analysis 
Esposito, C., Perugini, P., Accardo, A.F., Ricci, F 
Theoretical and Experimental Analysis of Composite Beams with Elastic Couplings 
Kaiser, C., Francescatti, D 
Stability and Elements Postbuckling Behaviour of Complex Composite 
Zamula, G.N., lerusalimsky, K.M 
Optimization of Rotating Disks via Genetic Algorithm 
Scaramuzzino, F 


SYSTEM DESIGN (Student Session)


Design Method for Marine Propeller/Stator Propulsors 
Alkan, A.D., Yilmaz, T., Guner, M 
High Performance Supersonic Aircraft Intake Design 
Haque, M.N., Ransom, E.C.P., Self, A 
Life Support System for Aircraft Crew 
Nicic, N.A 


WIND TUNNEL TECHNOLOGY


ETW  Flow Quality Aspects and First Model Tests 
Quest, J 
Cryogenic Model Technology for ETW 
Icart, G., Angeli, T., Dupriez, F. 
The Atmospheric Reentry Simulator in Naples 
Esposito, A., Monti, R., Zuppardi, G 
The Low Speed Tiltable Wind Tunnel SWT112 
Rosen, J., Nyström, T 


FLIGHT DYNAMICS OF LOW SPEED VEHICLES


Minimum LandingApproach Distance for a VUKT Sailplane 
Stefanovic, Z., Cvetkovic, D 
Preliminary Design of a Solar Powered Tailless Motorglider 
Guglieri, G., Quagliotti, F 
CenterofGravity and Lift Coefficient Limits of a Gliding Parachute Case Study 
losilevskii, G 


MULTIDISCIPLINARY DESIGN OPTIMIZATION


Technology Assessment with MultiDisciplinary Aircraft Design Tools on the Next Generation Supersonic Commercial Transport 
Reith, D. von 
Sensitivities and Integrated AerodynamicStructural Optimal Design 
Arsuffi, G., Mastroddi, F., Morino, L 
An Object Oriented Approach to Conceptual Aircraft Design through ComponentWise Modelling 
Schneegans, A., Haberland, Ch., Kokorniak, M., Domke, B 


ACTIVE VIBRATION CONTROL


Vibration Alleviation of a Hingeless Helicopter Rotor Blade by State Feedback 
Belo, E.M., Marques, F.D 
Active Control on Typical Helicopter Panels by using PiezoActuators 
De Vivo, L., Concilio, A 
Active Vibration Suppression Concepts for Buffet Excited Vertical Tails 
Schweiger, J., Simpson, J., Sensburg, O 


POSTBUCKLING OF COMPOSITES


Design, Analysis and Testing of a Postbuckling CoCured Composite Control Surface 
Scott, M.L., Cheung, A.K.H., Newman, P.D 
Buckling and PostBuckling Behaviour of Composite Cylindrical Shells 
Bisagni, C 
Postbuckling Behaviour of Graphite/Epoxy Wing Boxes Panels under Pure Torsion 
Romeo, G., Frulla, G 


UNSTEADY/VORTEX AERODYNAMICS


Unsteady Vortex Flow Phenomena on Delta Wings at High Angles of Incidence 
Mabey, D.G 
Fin Unsteady Surface Pressure Evaluation Due to Buffeting Based on Measured Fluctuating Velocities 
Breitsamter, C., Laschka, B 
An Analysis of Vortex Breakdown Predicted by the Euler Equations 
Strohmeyer, D., Orlowski, M., Longo, J.M.A., Hummel, D., Bergmann, A 
Calculation of Vortex Breakdown over Delta Wing by a VortexLattice Method 
Boffadossi, M 
Influence of Fuselage Shape on Single Fin Buffeting 
Chesneau, T.R., Wood, N.J 


HIGH SPEED AERODYNAMICS/LAUNCHERS


SpacePlanes and Launchers Aerodynamic Study with Euler and NavierStokes Computations 
Oswald, J., Bousquet, J.M 
Large Scale NavierStokes MultiBody Launch Vehicle Flowfield Simulations 
Wang, J.C.T., Taylor, S 
Sideslip Aerodynamics for Hytex Space Vehicle 
Sillen, M 
Numerical Investigations of the Flows around Various Cruciform WingBody Configurations at Mach Numbers from 2. to 10. and Arbitrary Angles of Attack using Sychev's Theory 
Voevodenko, N.V 


FLIGHT CONTROL II


Use of Neural Networks for Manoeuvre Load Control 
McLean, D 
Aileron to Rudder Interconnection with Analytical Redundancy 
Oliva, A.P 
Helicopter Inverse Simulation Incorporating an Individual Blade Rotor Model 
Rutherford, S., Thomson, D.G 
Development and Trials of an Autonomous Flight Control System for UAV's 
Valentinis, F., Bil, C., Riseborough, P 
AnalyticalComputational Method for Matching Optimal Control Formulations 
Ponzi, C 


SUBSONIC TRANSPORTS


Conceptual Design for Passenger Airplane of Very Large Passenger Capacity in Flying Wing Layout 
Denisov, V.E., Bolsunovsky, A.L., Buzoverya, N.P., Gurevich, B.I., Shkadov, L.M 
A Brief Comparison of Powered Lift, Flying Wing and Current Technology Subsonic Civil Transport Aircraft Concepts 
Kehayas, N 
Aerodynamic Design and Technology Concepts for a New UltraHigh Capacity Aircraft 
Greff, E 
The Application of the Wing Tip Lifting Surfaces for Practical Aerodynamic 
Kravchenko, S.A 


AEROELASTICITY


A Unified Boundary Integral Formulation for Acoustoaeroelastic Analysis of Shells 
lemma, U., Gennaretti, M., Trainelli, L., Morino, L., Giordani, A 
Investigation into the Applicability of Neural Network to Load Identification 
Cao, X., Mitsui, Y., Sugiyama, Y., Tang, J., Song, B 
Experiences with the Evaluation of the High Modal Density Structural Dynamics 
De Rosa, S., Marulo, F., Franco, F., Ricci, F 
VibroAcoustic Modelling of the Noise Transmission for the Saab 2000 
Goransson, P., Tengzelius, U 


DURABILITY AND DAMAGE TOLERANCE I


Scatter Factors for Damage Tolerance Justification 
Pizzanelli, L., Beaufils, J.Y., Duprat, D 
On Compression Creep of Metal Matrix Composite (Al 6061) at Elevated Temperatures 
Ismail, Y.M 
Transient Dynamic Analysis of the Damage Process of Laminated Composite Panels and Stiffened Panels due to Low Velocity Impact 
Guan, Z.D., He, Q.Z., Li, Z.N., Kou, C.H 
A Probabilistic Approach to Fatigue Damage Accumulation for Damage Tolerance and Durability of Ageing Aircraft 
Liao, M., Xu, X.F., Yang, Q.X 
The New Common Mathematical Model for Expressing Fatigue Characteristics of the Typical Airframe Structure Elements 
Maler, Z 


STRUCTURES AND MATERIALS (Student Session)


New Nondestructive Testing Method for Ageing Evaluation of Aircraft Structure 
Pirfo Barroso, S 
The Static and Dynamic Structural Analysis of an Amphibious Aircraft 
Faria, S.C., Canale, A.C 
Dynamics of OneDimensional Structures with DesignedIn Disorder 
Sayar, M., Demirel, M.C., Atilgan, A.R 


CFD DEVELOPMENT III


Adaptive Local Grid Refinement for Multiblock Solvers 
Amato, M., laccarino, G., Paparone, L 
An Improved CebeciSmith Turbulence Model for BoundaryLayer and NavierStokes Methods 
Cebeci, T., Chang, K.C 
Development and Application of Methods for Laminar Flow Research at ARA 
Wong, P.W.C., Maina, M 
Viscous Coupling Techniques using Unstructured and Multiblock Meshes 
Szmelter, J 
Numerical Investigation of Unstructured Grid Generation via Modified Bowyer's Method 
Wan, T 
An InverseDirect Hybrid NavierStokes Solver using PseudeAnalytic Functions 
Miyazaki, T 


AIRFOILS/HIGH LIFT


Requirements for Effective High Lift CFD 
Lynch, F.T., Potter, R.C., Spaid, F.W 
Modelling of Flow Past Body with Thick Wake in Classical Air Wing Theory 
Toison, F., Legallais, Ph., Hureau, J 
Aerodynamic Shape Optimization Based on HighLevel Physics 
Lee, K.D., Eyi, S 
Drag Reduction for Supercritical Aerofoils 
Sedaghat, A., Shahpar, S., Hall, I.M 
Numerical Simulation of InFlight Aircraft Icing 
Brahimi, M.T., Tran, P., Tezok, F., Paraschivoiu, I 
Prediction of LE and TE Devices Aerodynamics in HighLift Configurations with Mach and Reynolds Number Effects 
Nangia, R.K., Galpin, S.A 


FLIGHT AT HIGH ANGLE OF ATTACK II


Analysis of Aircraft Maximum Performances on Optimal Trajectories 
Avanzini, G., De Matteis, G., De Socio, L.M 
Modelling of Aeroplane Dynamics in Extreme Flight Conditions 
Sibilski, C 
Optimal Trajectory Analysis of High Angle of Attack Missiles 
Innocenti, M., Nasuti, F 
Method of Control of a Straked Wing Aircraft for Cobra Manoeuvres 
Dzygadlo, Z., Kowaleczko, G., Sibilski, K 
Tactical Utility of the X31A Using Post Stall Technologies 
Gutter, R., Friehmelt, H., Haiplik, R 


PROPULSION INSTALLATION AERODYNAMICS


Numerical and Experimental Analysis of the Effect of a Pusher Propeller on a Wing 
Catalano, F.M., Maunsell, M.G 
Scaling of ASTOVL Jet FlowFields 
Knowles, K 
NavierStokes Analysis for Engine Airframe Integration 
Chaput, E., Barrera, L., Gacherieu, C., Tourrette, L 
Afterbodies and Nozzles Optimization by using Inverse Methods 
Larocca, F 
On the Numerical Investigation of Inlet Buzz Flow 
Lu, P.J., Jain, L.T 


OPERATIONS


Airborne Systems Technology Application to the Windshear Threat 
Arbuckle, P.D., Lewis, M.S., Hinton, D.A 
Parametric Study of Performance of Aircraft Equipped with Airborne Reactive and Forward Looking Sensor during Microburst Encounter including Raining Effect 
Descatoire, F., Guffond, D., Huynh, H.T 
Electromagnetic Energy for the Prevention of Ice Deposition on Aircraft Surfaces 
Van Loock, W.M 
Flight Tests with Computer Generated Synthetic Vision for Improving Poor Visibility Operations 
Sachs, G., Dobler, K 
S.S.T.O. & T.S.T.O. LOX Collection System Performances: Influence of LOX Plant Architecture 
Hendrick, P 
ComputerAided Implementation of the "Duel" Airborne Operationally Consulting Expert System Investigative Prototype 
Romanova, V.D., Fedunov, B.E., lunevich, N.D 


CONFIGURATION AND DESIGN (Student Session)


Optimization of Regional Aircraft Configurations from Passengers' Perspective 
Pant, R 
Conceptual Design Methodologies for Flyingboats and Floatplanes 
Chicken, H.S 
Conceptual Design of an Aircraft for Australian Outback Conditions 
Roots, M 
Redesign and Construction of a High Performance Single Engine Aeroplane 
Waterhouse, J.R 
ATR/Vehicle Integration 
Christensen, K 


WIND TUNNEL TECHNIQUES


Helicopter Rotor Blade Aeroacoustics: A Comparison of ModelScale Wind Tunnel with FullScale Flight Test Results 
Heller, H., Buchholz, H., Schultz, K.J., Ahmed, S.R., Splettstoesser, W 
Investigation of the Airflow around Aircraft Model at High and Intermediate Angle of Attack with Pressure Sensitive Paint 
Bykov, A.P., Fonov, S.D., Mosharov, V.E., Orlov, A.A., Pesetsky, V.A., Radchenko, V.N 
Static and Forced Oscillation Tests on a Generic Combat Aircraft Model 
Weir, B., Walker, J.M 


UNSTEADY AERODYNAMICS II


A Transonic Doublet Lattice Method for General Configurations 
Zyl, L.H. van 
Further Refinement of the Nonplanar Aspects of the Subsonic DoubletLattice Lifting Surface Method 
Rodden, W.P., Taylor, P.F., McIntosh, Jr., S.C 
Unsteady Airloads Prediction for Oscillating Airfoils at Separated Flow Conditions 
Coiro, D.P., Pagano, A 


APPLICATIONS OF SIMULATION


The United States Air Force's Use of InFlight Simulation for Aeronautical Research 
Markman, S.R 
The Use of Simulation Tools in the Calculation of AircraftShip Interface Operational Limits 
De Ferner, B., Le Bihan, O 
Some Results of Piloted Simulator Investigations on Windshear Detection Systems and Icon Display Concepts 
Rouwhorst, W.F.J.A., Haverdings, H 


SAFETY


The Technical Development and Importance of Aircraft Recording Systems for Air Safety Investigation 
Mayes, P 
Failure Analysis and System Designing with Reliability and Safety taken into Consideration 
Borgon, J., Jazwinski, J., Woropay, M., Zurek, J 
Simple Analysis to Assess the Evacuation of Transport Airplanes 
MartfnezVal, R., Hernandez, C 
An Evaluation of Approach and Landing Factors Influencing Airport Safety 
Khatwa, R., Roelen, A.L., Karwal, A.K., Enders, J.H., Dodd, R., Tarrel, R 


SMART STRUCTURES


On the Optimal Placement of PZT Actuators for the Control of the Dynamic Response of a Beam 
Barboni, R., Fantini, E., Gaudenzi, P., Mannini, A 
Vibration and Shape Control of Smart Structures 
Huang, P.Z., Yang, S.M 
ModelIndependent Fuzzy Vibration Suppression of Flexible Structures using NonCollocated Transducers 
Cohen, K., Weller, T., BenAsher, J 


FLIGHT DYNAMICS I (Student Session)


The Robust Fault Diagnosis Based on the Singular Value Decomposition 
Hu, C.H., Xu, H.L., Oing, W 
AutoPilot CommandGenerator Tracker Design by LEQG/LTR Method 
Tsai, H.L., Lin, J.M., Chang, C.H 
Numerical Simulation of the Performance of Aerobatic Aircraft 
Csapb, G 


FLUID PHYSICS II


Eduction of Turbulent Structures in a Thermal Boundary Layer Flow 
luso, G., Onorato, M., Onorato, M 
Investigation into the Mixing Layer due to Two Parallel Supersonic Streams 
Tarnopolsky, A.Z., Gai, S.L 
Unsteady Base Flow  Vortex Shedding and Pressure Fluctuations 
Vassilopoulos, K., Gai, S.L 
The Effect of Offset Ratio on the Mean Flow Characteristics of Turbulent Offset Jets 
Nasr, A., Lai, J.C.S 
Momentum and Heat Transfer in Laminar Boundary Layer Flows of NonNewtonian PowerLaw Fluids Past External Surfaces 
Erim, M.Z., Yükselen, M.A 


COMBUSTION AND EMISSIONS


Experimental Studies on Atomization, Vaporization and Combustion for Liquid Rocket Propulsion 
Brummund, U., Cessou, A., Vogel, A 
Application of a Domain Decomposition Technique to the Mathematical Modelling of a Solid Fuel Combustion Chamber of a Ramjet 
Coelho, P.J., Duic, N., Carvalho, M.G 
Possibilities of Suppression Toxic Substances Emission by NonStationary Combustion 
Bazarov, V.G 
Status and Trends of Aeroengine Pollutant Emissions 
Hourmouziadis, J., Wulff, A 
Calculation of Turbulent Reacting Flows in a Cylindrical Combustor with Swirling Inflows 
Bai, X.S., Fuchs, L 


AIR TRAFFIC CONTROL


Information Processing Strategies in Air Traffic Controllers 
Amaldi, P., Boudes, N., Cellier, J.M 
The Flight Management System within WorldWide Communication/ Navigation/Surveillance and Air Traffic Management Applications 
Wittig, T., Dudek, H.L 
4D ATM Cockpit: SetUp and Initial Evaluation 
Hoogeboom, P.J., Huisman, H 
An Optimal Aircraft Conflict Resolution System Based on Hybrid Models 
Bousson, K., Paglione, P 


AEROELASTICITY II


Modeling of SemiEmpirical Transonic Unsteady Aerodynamics for Predicting Limit Cycle Oscillation Characteristics of Fighter Aircraft 
Meijer, J.J 
Influence of Structural Modifications on the Aeroelastic Analysis of Large Transport Aircraft 
Balis Crema, L., Mastroddi, F., Coppotelli, G., lazzetta, A., Pecora, M 
Robust Stabilization of a Transonic Flutter based on a Linearized Transonic Math Model 
Matsushita, H., Saitoh, K., Hashidate, M 
Optimization of Composite Aeroelastic Wings using a Cellular Automata Paradigm 
Persiani, F., Piancastelli, L 
Largely Bent Wing Flutter 
Avertchenkov, V.V 


DURABILITY AND DAMAGE TOLERANCE II


The Effects of Surface Corrosion on the Fatigue Behaviour of Aluminium Alloy Specimens Containing Cold Expanded Holes 
Glinos, N., Wagstaff, P.G., Cook, R 
Effect of Material Properties and Load Parameters on the Crack Growth Propagation 
Behai, J., Dlouhä, J., Ruzek, R 
A Theoretical Approach for the Damage Behaviour Characterisation of Composite Shells 
Ikonomopoulos, G., Perreux, D., Marchetti, M 
Studies on the Durability of Polymeric Materials for High Performance Composites 
Grayson, M.A 
The Prediction of Defects of A/C Pressing 
Calkovsky, A., Samek, R 
A Comparative Evaluation of Damage Influence on Aircraft Structure Safety 
Danilecki, S 


FLIGHT DYNAMICS II (Student Session)


Experimental Study of Aircraft Stability Enhancement at High Angles of Attack 
Huang, A 
Calculation of Aerodynamic Coefficients of Missile Like Geometries by Viscous/lnviscid Coupling 
Onen, C., Yavuz, I., Kavsaoglu, M.S 
Method for the Evaluation Vertical Tail Surfaces of a Light Aircraft Based on Lateral Flying Qualities 
Memon, G 
Steeper Approaches 
Rhodes, D.P 


CFD DEVELOPMENT IV


A Pure Vortex Method for Simulating Unsteady, Incompressible, Separated Flows Around Static and Pitching Aerofoils 
Lin, H.Q., Vezza, M 
Application of Viscouslnviscid Interaction Methods for a Separated Flow Calculation about Airfoils and HighLift Systems 
Lyapunov, S.V., Woikov, A.V 
An Accurate and Efficient Viscous Interaction Approach for Analysis and Design of Airfoils and HighLift Configurations 
Verhoff, A., Michal, T., Cebeci, T 
Convective Discretization Dependence on the Performance of Several Turbulence Models for Airfoil Stall Flow 
Kobayashi, M.H., Marques, N.P.C., Pereira, J.C.F 
Calculation of HighLift Aerodynamics on Adaptive Unstructured Grids 
Jahangirian, A.R., Johnston, L.J 
A Block Structured Based Method for the Flow Prediction over Low Reynolds Numbers MultiElement Airfoils 
Wilquem, F., Passelecq, C. Degrez, G 


FLOW CONTROL


Linear Control of Side Forces and Yawing Moments using the Dynamic Manipulation of Forebody Vortices 
Lee, R., Hanff, E.S., Kind, R.J 
Behaviours of LeadingEdge Separation Vortex Formed on a Delta Wing with Vortex Flaps 
Rinoie, K., Fujita, T., Iwasaki, A., Fujieda, H 
Effect of Forebody Form on the Aerodynamic Charateristics and Airflow around an Aircraft Model up to High Angles of Incidence 
Pesetsky, V., Kalashnikov, S., Lovell, D.A 
Effect of Lateral Blowing on Aerodynamic Characteristics of Low AspectRatio Wings at High Angles of Attack 
Karashima, K., Sato, K 
Aerodynamic Characteristics of a Highly Swept Wing in Steady/Unsteady Pitching States and Effects of Flap Control at Large Incidence 
Hsing, T.D., Yu, G.Z., Gu, Z.F 
Experimental Measurement on Airfoils with Trailing Edge Wedges 
Sardjadi, D 
Study of a Local Surface MicroDisturbance Effects on the Supercritical Airfoil Performance 
Kania, W 
WINGGRID, A Novel Device for Reduction of Induced Drag on Wings 
La Roche, U., Palffy, S 


HYDRAULIC ACTUATION/FLIGHT CONTROL


ComputerAided Engineering for the Design of Flight Control and Hydraulic Systems 
Scholz, D 
Effects of Anomalies in Hydraulic Actuators into Dynamics of the Aircraft Control Systems 
Rohacs, J 
A Critical Comparison between Different Methods of Flap Systems Actuation Speed Limitation 
Borello, L., Villero, G., D'Onofrio, E 
About Aeroservoelasticity Criteria for Electrohydraulic Servomechanisms Synthesis 
Ursu, I., Vladimirescu, M., Ursu, F 
Computer Analysis and Simualtion of Transient State and Pressure Recovering in Fast Cyclic Hydraulic Actuators 
Jankovic, J 
Digital Redesign of the NRC Bell 205 Artificial Feel System 
Gubbels, A.W., Goheen, K.R 


TURBOPROP INTEGRATION


Numerical Study of Aerodynamic High Speed Propeller Engine Integration on Transport Aircraft 
Colin, P., Moreux, V., Barillier, A 
Experimental Investigation on Propeller Slipstream Interference Effects on a Swept Wing at Low Speed Conditions 
Prijo Kusumo, J., Gayus, N., Custers, L.G.M., Haij, L.H. de, Veldhuis, L.L.M 
Analysis of Propeller Slipstream Effects on a Trailing Wing 
Veldhuis, L.L.M 
Measurements of the Propeller Slipstream Interaction with a Nacelle and Wing 
Barber, D.J., Nelson, T.E 
Analysis of Propeller Slipstream Field 
Wang, D.Q., Lindblad, I., Eliasson, P 


STRUCTURAL DYNAMICS


Nonlinear Vibration Tests of Isotropic Cylindrical Shells under Compressive Axial Loads 
Gunawan, L., Klompä, A.W.H., Zwaan, R.J 
Behaviour of an Aeronautic Composite Panel submitted to an Impulsive Loading 
Moreno, A., Dauce, J.P 
Vibrations and Stability of a BiselfExcited Surface Structure in Supersonic Flow Subjected to a Follower Force 
Dzygadlo, Z., Nowotarski, I., Olejnik, A 
Effects of Replacement of a Dynamic Crash Test with a Quasi Dynamic One. Test of the PW5 World Class Glider 
Czarnocki, P., Wiacek, T., Wingralek, W 
The Application of Dynamic Loads to a Full Scale F/A18 Fatigue Test Article 
Conser, D.P., Graham, A.D., Smith, C.J., Yule, C.L 


INTERNAL FLOWS AND HEAT TRANSFER


The Interaction between Secondary Flow and Film Cooling in a Turbine Nozzle 
Langowsky, C 
The Influence of Rotation and Buoyancy on Radially Inward and Outward Directed Flow in a Rotating Circular Coolant Channel 
Elfert, M., Hovel, H., Towfighi, K 
Flow Separation Prediction on Inlets with Mach and Reynolds Number Effects in Subsonic Flight 
Nangia, R.K., Palmer, M.E., Hodges, J 
Validation of NonAxisymmetric Terms in 3D Viscous Flow Analysis for High Speed Axial Compressors 
Kaldellis, J.K., Georgantopoulos, G.A 
Heat Transfer around a 180deg Turn in a Square Channel 
Carlomagno, G.M., Cardone, G., Astarita, T 


AERODYNAMICS III (Student Session)


Analysis of WrapAround Finned Missiles with a Zonal NavierStokes Solver 
Sen, T.S., Korkem, B., Temel, B., Kavsaoglu, M.S 
Aerodynamic Design of Swept Infinite Wing with Flap for Subsonic and Transonic Flight Regimes 
Kovalev, K.V 
Aircraft Induced Drag Minimization Using the Constrained Optimization Method 
Martins, A.L., Ribeiro, R.S 
Numerical Solution of Axisymmetric JetPlume Coupled with External Freestream 
Yilmaz, E., Kavasaoglu, M.S 
Developed CAI Model for Complex Parts 
Zivkovic, S 


AIRCRAFT AERODYNAMICS


NavierStokes Calculations for a Complete Aircraft 
Lehtimaki, R., Laine, S., Siikonen, T., Salminen, E 
JoinedWing Configuration Aerodynamics 
Wai, J.C., Herling, W.W., Roetman, E.L 
Investigation of the Vortex Wake Evolution and Flight Safety 
Vyshinsky, V.V., Soudakov, G.G 


UNSTEADY AERODYNAMICS III


The Unsteady Pressure Field on a Wing with Large Regions of Separated Flow 
Lee, B.H.K., MarineauMes, S 
Unsteady Aerodynamic Phenomena on Novel Wing Planforms 
Woods, M.I., Wood, N.J 
The Comparison between the Dynamic Stall of a Finite Wing with Straight and Swept Tips 
Galbraith, R.A.McD., Coton, F.N., Jiang, D., Gilmour, R 


FLIGHT CONTROL III


Rate Limiters with Phase Compensation 
Rundqwist, L 
Robust Autopilot Design Strategy for Functionally Dependent Parameter Uncertainties 
Shaviv, G.E., Idan, M 
InFlight Monitoring of Critical Sensors 
Jann, Th 


LANDING GEAR


Landing Gear Integration on a Supersonic Transport Aircraft 
Roloff, G 
SemiActive Controlled Shock Absorber for Large Flexible Aircraft 
Wentscher, H., Roloff, G 
The Simulation of Aircraft Landing Gears During Usual and Unusual Manoeuvres 
Kapadoukas, G.G., Self, A.W., Marteau, F 
WellConditioned Procedures for Optimal Robust Design of Flight Control Systems 
Stoica, A 


BUCKLING BEHAVIOUR


Buckling Behaviour of Large GLARE Fuselage Shells under Compression and Shear Loading 
Horst, P 
Postbuckling of Laminated Composite and SandwichType Plates and Shells: On the Significance of the Fulfillment of Static Interlayer Continuity Conditions 
Librescu, L., Lin, W., DiSciuva, M., Icardi, U 
Application of SkewTransverseiyRepetitive Analysis for Buckling of Plate Arrays with Curved or Straight Internal Supports 
York, C.B 




The International Council of the Aeronautical Sciences 



ICAS Program Committee 

ICAS Member Associations 
