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- Experimental Results With Airfoils Tested in the High-Speed Tunnel at Guidonia
- Supersonic-tunnel tests of projectiles in Germany and Italy
- Completed Tabulation in the United States of Tests of 24 Airfoils at High Mach Numbers (Derived From Interrupted Work at Guidonia, Italy in the 1.31- by 1.74-Foot High-Speed Tunnel)
- Application of the Method of Characteristics to Supersonic Rotational Flow
- Preliminary Investigation of a New Type of Supersonic Inlet
- Application of the Method of Characteristics to Supersonic Rotational Flow
- Theoretical and Experimental Analysis of Low-Drag Supersonic Inlets Having a Circular Cross Section and a Central Body at Mach Numbers of 3.30, 2.75, and 2.45
- The Method of Characteristics for the Determination of Supersonic Flow Over Bodies of Revolution at Small Angles of Attack
- Theoretical and Experimental Analysis of Low-Drag Supersonic Inlets Having a Circular Cross Section and a Central Body at Mach Numbers 3.30, 2.75, and 2.45
- Method for evaluating from shadow or Schlieren photographs the pressure drag in two-dimensional or axially symmetrical flow phenomena with detached shock
- The method of characteristics for the determination of supersonic flow over bodies of revolution at small angles of attack
- Preliminary Analysis of Axial-Flow Compressors Having Supersonic Velocity at the Entrance of the Stator