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 II.

摘要

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.