Accession Number : AD0472298


Title :   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


Descriptive Note : Workshop Proceedings


Corporate Author : ARO INC ARNOLD AFS TN


Personal Author(s) : Welsh, C J ; Chapman, Gary T ; Platou, Anders S ; Covert, Eugene E ; Regan, Frank J ; Ward, L K ; Rightley, E C ; Dayman, Jr , Bain ; Prislin, R H


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/472298.pdf


Report Date : Jan 1965


Pagination or Media Count : 288


Abstract : 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.


Descriptors :   *AERONAUTICAL LABORATORIES , *SYMPOSIA , DAMPING , ELECTROMAGNETIC DRIVES , OSCILLATION , SURFACE TEMPERATURE , WIND TUNNELS , STABILITY , ABLATION , ANGLE OF ATTACK


Subject Categories : Aerodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE