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- Theoretical aerodynamic coefficients of two-dimensional supersonic biplanes
- Load distributions due to steady roll and pitch for thin wings at supersonic speeds
- Approximate method for predicting form and location of detached shock waves ahead of plane or axially symmetric bodies
- Experimental investigation of supersonic flow with detached shock waves for Mach numbers between 1.8 and 2.9
- Flow separation ahead of a blunt axially symmetric body at Mach numbers 1.76 to 2.10
- Preliminary investigation of use of conical flow separation for efficient supersonic diffusion
- Interaction of oblique shock waves with regions of variable pressure, entropy, and energy
- Use of aerodynamic heating to provide thrust by vaporization of surface coolants
- Estimation of inlet lip forces at subsonic and supersonic speeds
- Some effects of bluntness on boundary-layer transition and heat transfer at supersonic speeds
- Some effects of bluntness on boundary-layer transition and heat transfer at supersonic speeds
- Oblique-shock relations at hypersonic speeds for air in chemical equilibrium
- Composition and thermodynamic properties of air in chemical equilibrium