Accession Number : ADA157215


Title :   Air Force Academy Aeronautics Digest.


Descriptive Note : Final rept.,


Corporate Author : AIR FORCE ACADEMY CO


Personal Author(s) : DeJongh,J E ; Heiser,W H ; Hale,M


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a157215.pdf


Report Date : Apr 1985


Pagination or Media Count : 269


Abstract : 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.


Descriptors :   *AERONAUTICS , CONTROL , FLIGHT TESTING , MEASUREMENT , PITCH(MOTION) , DETECTORS , AIRCRAFT , MILITARY AIRCRAFT , FLIGHT CONTROL SYSTEMS , INTERACTIONS , COMPUTERS , DYNAMICS , THEORY , RATES , AIRFOILS , STALLING , LIMITATIONS , AERODYNAMIC FORCES , DRAG , AMPLITUDE , THRUST , WIND TUNNELS , FINS , AERODYNAMICS , DIGITAL FILTERS , UNITED STATES AIR FORCE ACADEMY , PIVOTS


Subject Categories : Aircraft
      Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE