Note on the Structural Failure of Handley Page 88 (E6/48) VX.330
Evaluation of Aircraft Accessory Power Transmission Systems by Selected Analytical Methods
Evaluation of Aircraft Accessory Power Transmission Systems by Selected Analytical Methods
Research and Development in the Field of High Altitude Plastic Balloons
Final Report (Balloon Launching)
Structural Design for Aerodynamic Heating. Part II. Analytical Studies
Standard Atmosphere-Tables and Data for Altitudes to 65,800 Feet
Optimum Vs Correlation Methods in Tracking Random Signals in Background Noise
Recent Climatic Fluctuations in Maritime Provinces
Metabolic Cost of Load-Carrying: A Discussion of Experimental Findings
A note on the ability to predict transonic drag-rise changes due to model modifications
Generalized Missile Dynamics Analysis. III. Aerodynamics
Launching of Airborne Missiles Underwater. Part II. Response to Sea and Swell
The Variation of Heating Rates in a 1/30 Scale Booster Rocket Exhaust Jet
Determination of the Velocity Field of an Airfoil with Leading Edge Suction
High-Altitude Wind Measurements
Application of Meteorological Rocket Systems
Structural Considerations of Inflatable Reentry Vehicles
Rocket Sounding of High Atmosphere Meteorological Parameters
Aerodynamic Analysis of a Low Density Hypersonic Shock-Wind Tunnel
Transonic and Supersonic Flutter Trend Investigation of a Variable-sweep Wing
Transonic and Supersonic Flutter Trend Investigation of a Variable-Sweep Wing
Examination of Future Trends in Short Range Passenger Air Transportation
Experience in Data Collection. Vii. Naval Ship Material Classification
Design and Construction of a Lunar Seismograph Progress Report No. 10, 1 Oct. - 31 Dec. 1961
Transonic Flutter Investigation of Models of a Proposed Variable-Sweep Wing
Aerodynamic analysis of tektites and their parent bodies
Aerodynamic Analysis of Tektites and Their Parent Bodies