Search U.S. government technical reports digitized or harvested by TRAIL.
Rolling Effectiveness of a Thin Tapered Wing Having Partial-Span Ailerons as Determined by Rocket-Powered Test Vehicles
The Rolling Effectiveness of Wing-Tip Ailerons as Determined by Rocket-Powered Test Vehicles and Linear Supersonic Theory
Free-Flight Investigation of the Longitudinal Stability and Control of a Rocket-Propelled Missile Model Having Cruciform, Triangular, Interdigitated Wings and Tails
Aerodynamic Characteristics of Bodies at Supersonic Speeds: A Collection of Three Papers
Effect on Transonic and Supersonic Drag of a Fuselage Protuberance of an Essential Unswept Wing-Fuselage Combination
Similitude Relations for Free-Model Wind-Tunnel Studies of Store-Dropping Problems