Contents: The Seven-Hole Pressure Probe; Wind Tunnel Study on the Drag Effects of an Aft-Mounted Ventral Fin on a T-38 Model; An Experimental Investigation of an Airfoil Undergoing Large Amplitude Pitching Motions; Interrelated Effects of Pitch Rate and Pivot Point on Airfoil Dynamic Stall; An Examination of Curve Smoothing Using Digital Filter Theory; Flight Test Measurement of the Aerodynamic Effect of Thrust Level on Lift and Drag; Flight Control System Design for a Computer Controlled Aircraft with Limited Sensors.
Air Force Academy Aeronautics Digest
1985
269 pages
Report
Keine Angabe
Englisch
Aeronautics & Aerodynamics , Aeronautics , Aerodynamic forces , Aircraft , Airfoils , Amplitude , Computers , Control , Detectors , Digital filters , Drag , Dynamics , Fins , Flight control systems , Flight testing , Interactions , Limitations , Measurement , Pitch(Motion) , Pivots , Rates , Stalling , Theory , Thrust , United states air force academy , Wind tunnels , Military aircraft , Aerodynamics
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