Air Force Academy Aeronautics Digest.
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1985
- Accession Number
- ADA157215
Entities
People
- J. E. Dejongh
- Matthew Hale
- W. H. Heiser
Organizations
- United States Air Force Academy