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- Experimental investigation of hot-gas bleedback for ice protection of turbojet engines 1: nacelle with offset air inlet
- Investigation of the Penetration of an Air Jet Directed Perpendicularly to an Air Stream
- Experimental investigation of hot-gas bleedback for ice protection of turbojet engines 2: nacelle with long straight air inlet
- Penetration of Air Jets Issuing from Circular, Square, and Elliptical Orifices Directed Perpendicularly to an Air Stream
- Experimental Investigation of Effect of Jet Exit Configuration on Thrust and Drag
- NACA Investigations of Icing-Protection Systems for Turbojet-Engine Installations
- A General Correlation of Temperature Profiles Downstream of a Heated-Air Jet Directed Perpendicularly to an Air Stream
- Analytical Investigation of Icing Limit for Diamond-Shaped Airfoil in Transonic and Supersonic Flow
- A Method for Rapid Determination of the Icing Limit of a Body in Terms of the Stream Conditions
- Analogy Between Mass and Heat Transfer with Turbulent Flow
- Investigation of Noise Field and Velocity Profiles of an Afterburning Engine
- Investigation of noise field and velocity profiles of an afterburning engine
- Investigation of Jet-Engine Noise Reduction by Screens Located Transversely Across the Jet
- Investigation of Far Noise Field of Jets 1: Effect of Nozzle Shape
- Near Noise Field of a Jet-Engine Exhaust
- Far Noise Field of Air Jets and Jet Engines