An Experimental Investigation at Mach Numbers from 2.1 to 3.0 of Circular-internal-contraction Inlets with Translating Centerbodies
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Mossman, Emmett A↗
Engineering topics
Pfyl, Frank A
Publications and source records attributed to Pfyl, Frank 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↗
Effect of Boundary-layer Control and Inlet Lip Shape on the Performance of a Twin-scoop Air-induction System at Mach Numbers from 0 to 1.9
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LAZZERONI FRANK A↗
A Study of a Symmetrical, Circular, Internal Compression Inlet
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Mossman, Emmet A↗
Experimental Investigation at Mach Numbers from 0 to 1.9 of Trapezoidal and Circular Side Inlets for a Fighter-type Airplane
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Mossman, Emmett A↗
An Experimental Investigation of the Air-flow Stability of a Scoop-type Normal-shock Inlet
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Mossman, Emmet A↗
Effects of Leading-edge Chord Extensions and an All-movable Horizontal Tail on the Aerodynamic Characteristics of a Wing-body Combination Employing a Triangular Wing of Aspect Ratio 3 Mounted in a High Position at Subsonic and Supersonic Speeds
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Wetzel, Benton E↗
Experimental Investigation of Aerodynamically Balanced Trailing-edge Control Surfaces on an Aspect Ratio 2 Triangular Wing at Subsonic and Supersonic Speeds
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Boyd, John W↗
Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness of an inboard elevon as a longitudinal- and lateral-control device at subsonic and supersonic speeds
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Pfyl, Frank A↗