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Flugmechanik
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1/10 Scale Model Test of a Fixed Chute Mixer-Ejector Nozzle in Unsuppressed Model, Part 1
2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
2-Dimensional Smoke Tunnel Tests of a Fairchild Aircraft Division Wagner 1 B Model
2nd AIAA Aeroelastic Prediction Workshop: Plans & an Interesting Technical Issue
5TH International Symposium: Small Satellites Systems and Services
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)