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- Free-Flight Investigation of the Zero-Lift Drag of Several Wings at Supersonic Mach Numbers Extending to 2.6
- Drag Measurements at Low Lift of a Four-Nacelle Airplane Configuration Having a Longitudinal Distribution of Cross-Sectional Area Conductive to Low Transonic Drag Rise
- Drag Measurements at Low Lift of a Four-Nacelle Airplane Configuration Having a Longitudinal Distribution of Cross-Sectional Area Conducive to Low Transonic Drag Rise
- The Effect of Some Surface Roughness Elements on the Drag of a Body of Revolution at Supersonic Speeds
- Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5
- Drag near zero lift of a 1/7-scale model of the Convair B-58 external store as measured in free flight between Mach numbers of 0.8 and 2.45
- Drag at model trim lift of a 1/15-scale Convair B-58 supersonic bomber
- Drag at Model Trim Lift of a 1/15-Scale Convair B-58 Supersonic Bomber
- Exploratory Tests of the Behavior of Several Materials in a Supersonic Air Jet at 4,000 Degrees Fahrenheit
- Some Experimental Heating Data on Convex and Concave Hemispherical Nose Shapes and Hemispherical Depressions on a 30-Degree Blunted Nose Cone
- Behavior of Some Materials and Shapes in Supersonic Free Jets at Stagnation Temperatures Up to 4,210 Degrees F, and Descriptions of the Jets