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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

Application of the Method of Characteristics to Supersonic Rotational Flow

Preliminary Investigation of a New Type of Supersonic Inlet

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

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 of 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


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