Preliminary Flight Measurements of the Total- Pressure Recovery of a Split-Wing Ram-Jet Inlet at Mach Numbers from 1.4 to 3.16
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Hinners, A. H., Jr.↗
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Results for “PRESSURE RECOVERY”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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An Experimental Investigation at Low Speeds of the Effects of Lip Shape on the Drag and Pressure Recovery of a Nose Inlet in a Body of Revolution
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Blackaby, James R↗
A Method for Evaluating the Effects of Drag and Inlet Pressure Recovery on Propulsion-system Performance
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Kremzier, Emil J↗
Flight Determination of the Drag and Pressure Recovery of an NACA 1-40-250 Nose Inlet at Mach Numbers from 0.9 to 1.8
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Sears, R I↗
Low-speed Investigation of the Effects of Angle of Attack on the Pressure Recovery of a Circular Nose Inlet with Several Lip Shapes
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Blackaby, James R↗
Preliminary Investigation of a Submerged Air Scoop Utilizing Boundary-layer Suction to Obtain Increased Pressure Recovery
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Nichols, Mark R↗
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↗
Pressure Recovery at Supersonic Speeds Through Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer II : Effect of an Oblique Shock Wave Immediately Ahead of the Inlet
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Brajnikoff, George B↗
Preliminary Investigation of a Submerged Air Scoop Utilizing Boundary-layer Suction to Obtain Increased Pressure Recovery
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Nichols, Mark R↗
Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8
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Sears, R I↗
Preliminary Data on the Effect of Body-nose Bluntness on the Drag and Pressure Recovery of a Side-inlet-body Combination at Mach Numbers of 1.4 and 1.7
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Stroud, John F↗
Flight Determination of Drag and Pressure Recovery of a Nose Inlet of Parabolic Profile at Mach Numbers from 0.8 to 1.7
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Sears, Richard I↗
Subsonic Mach and Reynolds Number Effects on the Surface Pressures, Gap Flow, Pressure Recovery, and Drag of a Nonrotating NACA 1-series E-type Cowling at an Angle of Attack of 0 Degrees
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Reynolds, Robert M↗
Effects of inlet wall contour on the pressure recovery of a 10 degrees 10-inch-inlet-diameter conical diffuser
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Copp, Martin R↗
Transonic Flight Tests to Determine Zero-lift Drag and Pressure Recovery of Nacelles Located at the Wing Tips on a 45 Degree Sweptback Wing and Body Combination
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Hoffman, Sherwood↗
Pressure Recovery, Drag, and Subcritical Stability Characteristics of Three Conical Supersonic Diffusers at Stream Mach Numbers from 1.7 to 2.0
A study of a 20 degree and a 25 degree half-angle high mass-flow ratio conical supersonic inlet was made on a 16-inch ram jet in the 8- by 6-foot supersonic tunnel. A greater range of stable subcritical operation was obtained with the low mass-flow ratio inlets; a greater range was obtained with the 25 degree than with the 20 degree half-angle low mass-flow ratio inlet. The high mass-flow ratio inlet had the least drag.
DIFFUSERS, SUPERSONIC↗
A proposed ram-jet control system operated by use of diffuser pressure recovery
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Faget, Maxime A↗
Total-pressure recovery characteristics of a model of the McDonnell XF3H-1 inlets and forebody in a free jet at a Mach number of 1.55
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Merlet, Charles F↗