The Change with Mass-flow Ratio of the Cowl Pressure Drag of Normal-shock Inlets at Supersonic Speeds
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Davis, Wallace F↗
Engineering topics
Davis, Wallace F
Publications and source records attributed to Davis, Wallace F.
Aerodynamic principles for the design of jet-engine induction systems
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Davis, Wallace F↗
Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area IV : Some Effects of Internal Duct Shape upon an Inlet Enclosing 37.2 Percent of the Forebody Circumference
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Davis, Wallace F↗
An Experimental Investigation at Supersonic Speeds of Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer
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Davis, Wallace F↗
Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area III : Inlet Enclosing 37.2 Percent of the Maximum Circumference of the Forebody
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Davis, Wallace F↗
Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area II : Effects of Slots upon an Inlet Enclosing 61.5 Percent of the Maximum Circumference of the Forebody
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Goldstein, David L↗
Pressure Recovery at Supersonic Speeds Through Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer I : Addition of Energy to the Boundary Layer
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Davis, Wallace F↗
Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area I : an Inlet Enclosing 61.5 Percent of the Maximum Circumference of the Forebody
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Davis, Wallace F↗
Comparison of various methods for computing drag from wake surveys
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EQUATIONS - DRAG, PROFILE - WRIGHT↗