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Flugmechanik
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1/5 Scale Model of Aeromot 200S SuperXimango for Scaled Flight Research
1/10 Scale Model Test of a Fixed Chute Mixer-Ejector Nozzle in Unsuppressed Model, Part 1
1 A Method of Flow Measurement About Full-Scale and Model-Scale Vehicles
2-D Airfoil Wind Tunnel Test at Stall
2D AND 3D INTAKES PERFORMANCE AND DRAG OF CRUISE M=1.6 CIVIL AIRCRAFT
2-D and 3-D mixing flow analyses of a scramjet-afterbody configuration
2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
2-D Circulation Control Airfoil Benchmark Experiments Intended for CFD Code Validation
2-Dimensional Smoke Tunnel Tests of a Fairchild Aircraft Division Wagner 1 B Model
2D Numerical Study of Synthetic Jets in Quiescent Flow
2D Unsteady Motion of a Flat Plate: Implementation and Model Simplification
2nd AIAA Aeroelastic Prediction Workshop: Plans & an Interesting Technical Issue
2nd AIAA Aeroelastic Prediction Workshop: Plans & an Interesting Technical Issue
3D Computational Studies of Flapping Wing in Frontal Gusty Shear Flow
3D DES Unsteady Simulation of Transonic Cavity Flows
3D Euler Calculations of Multibladed Rotors in Hover: Investigation of the Wake Capturing Properties
3D FINITE ELEMENT MODELING OF SINGLE-LAP SHEAR BOLTED JOINTS
3D Flow Field Investigations on Flapping Wing Aerodynamics (AIAA 2014-2879)
3D flyable curves for an autonomous aircraft
3-D Inlet Shock-Boundary Layer Interactions - PIV Database for the Second SBLI Workshop
3-D Navier-Stokes Analysis of Blade Root Aerodynamics for a Tiltrotor Aircraft In Cruise
3D-PTV Using Genetic Algorithm
3-D Simulation of Flexible Hypersonic Vehicles
3-D viscous flow CFD analysis of the propeller effect on an advanced ducted propeller subsonic inlet
5-Degree-of-Freedom Dynamic Rig for Wind Tunnel Tests of Aerospace Vehicles
5TH International Symposium: Small Satellites Systems and Services
6 degrees of freedom simulation of an unguided sounding rocket using Matlab/Simulink
8 m x 6 m Low Speed Wind Tunnel at the Chinese Aerodynamic Research and Development Center
13b. Debris and Re-Entry Burnout of Spacecraft
13ft 9ft Low Speed Wind Tunnel Facility at DRA (Aerospace Division) Bedford (UK)
70 Years of Aeropropulsion Research at NASA Glenn Research Center
82° Inclination Debris Cloud Revealed by Radar
100 LBS TO Low Earth Orbit (LEO): Small-Payload Launch Options
1988 Chevrolet/GMC Full-Size Pickup Truck Aerodynamics
1991 International Aerospace and Ground Conference on Lightning and Static Electricity, Volume 1
1993 Federal Aviation Administration Plan for Research, Engineering and Development