TRANSACTIONS OF THE SECOND TECHNICAL WORKSHOP ON DYNAMIC STABILITY TESTING, HELD AT THE ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AIR FORCE STATION, TENNESSEE ON APRIL 20-22, 1965. VOLUME 2
ARO INC ARNOLD AFS TN
Pagination or Media Count:
Contents Facilities, Techniques and Test Results Dynamic Stability Testing in the 1,000-ft Hypervelocity Range at the Arnold Engineering Development Center Problems Associated with Obtaining Accurate Dynamic Stability Results from Free-Flight Tests Free Flight Wing Tunnel Techniques at the Ballistic Research Laboratories Dynamic stability Testing with Magnetic Balance Systems Instrumentation and Techniques Used at the Naval Ordnance Laboratory for the Determination of Dynamic Derivatives in the Wind Tunnel Influence of Boundary Layer Transition on Dynamic Stability at Hypersonic Speeds Dynamic Stability Derivatives for a 10 Deg Blunt Cone at Mach Numbers from 0.5 to 21 Effect of a Hemispherical Aterbody on the Dynamic Stability of a Slender Cone Wind Tunnel Free-Flight Technique Free-Flight Cone Dynamic Stability Testing at High Amplitudes of Oscillation Consideration for Flow Hysteresis and Model Wall Temperature Effects on the Flow Field Dynamic Stability Testing Techniques at the Jet Propulsion Laboratory Free-Flight Technique for Measuring Dynamic Stability of Ablating Models Dynamic Stability Testing of Special Weapon Shapes and The Design and Performance of a Dynamic Model Drive System.