A Study of Several Theoretical Methods for Computing the Zero-lift Wave Drag of a Family of Open-nosed Bodies of Revolution in the Mach Number Range of 2.0 to 4.0
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Presley, Leroy L↗
Engineering topics
Mossman, Emmet A
Publications and source records attributed to Mossman, Emmet A.
Fuselage Side Inlets : a Study of Some Factors Affecting Their Performance and a Comparison with Nose Inlets
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Mossman, Emmet A↗
A Study of a Symmetrical, Circular, Internal Compression Inlet
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Mossman, Emmet A↗
An Experimental Investigation of the Air-flow Stability of a Scoop-type Normal-shock Inlet
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Mossman, Emmet A↗
The Effect of Lip Shape on a Nose-inlet Installation at Mach Numbers from 0 to 1.5 and a Method for Optimizing Engine-inlet Combinations
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Mossman, Emmet A↗
A Comparison of Two Submerged Inlets at Subsonic and Transonic Speeds
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Mossman, Emmet A↗
Effect of pressure recovery on the performance of a jet-propelled airplane
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AIRPLANES, JET - PERFORMANCE↗
An experimental investigation of the design variables for NACA submerged duct entrances
Information concerning the parameters and design variables affecting an NACA submerged duct design is presented.
Mossman, Emmet A↗
Development of NACA Submerged Inlets and a Comparison with Wing Leading-Edge Inlets for a 1/4-scale Model of a Fighter Airplane
Characteristics of NACA submerged duct entries and wing leading-edge inlets designed for a 1/4 scale flow model of a fighter-type airplane powered by a jet engine in the fuselage are presented.
DUCTS - PRESSURE RECOVERY↗