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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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At least 91 records · Page 5

All sources NASA NTRS DOE OSTI

NASA NTRS1948

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↗

NASA NTRS1948

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↗

NASA NTRS1948

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↗

NASA NTRS1948

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↗

NASA NTRS1949

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↗

NASA NTRS1950

Effect of Inlet Temperature and Humidity on Thrust Augmentation of Turbojet Engine by Compressor-inlet Injection

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Shillito, Thomas B↗

NASA NTRS1951

Force and Pressure Characteristics for a Series of Nose Inlets at Mach Numbers from 1.59 to 1.99 I : Conical Spike All-external Compression Inlet with Subsonic Cowl Lip

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Esenwein, Fred T↗

NASA NTRS1951

Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 II : isentropic-spike all-external compression inlet

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Obery, L J↗

NASA NTRS1951

Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 III : conical-spike all-external-compression inlet with supersonic cowl lip

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Weinstein, Maynard I↗

NASA NTRS1951

Preliminary Investigation of a Submerged Inlet and a Nose Inlet in the Transonic Flight Range with Free-fall Models

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Selna, James↗

NASA NTRS1951

Altitude-test-chamber Investigation of Performance of a 28-inch Ram-jet Engine IV : Effect of Inlet-air Temperature, Combustion-chamber-inlet Mach Number, and Fuel Volatility on Combustion Performance

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Kahn, Robert W↗

NASA NTRS1951

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↗

NASA NTRS1951

Force and Pressure Characteristics for a Series of Nose Inlets at Mach Numbers from 1.59 to 1.99 IV : Conical-spike External-internal Compression Inlet Utilizing Perforated Cowl

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Madden, Robert T↗

NASA NTRS1951

Comparison of Drag, Pressure Recovery, and Surface Pressure of a Scoop-type Inlet and an NACA Submerged Inlet at Transonic Speeds

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Frank, Joseph L↗

NASA NTRS1951

Preliminary Investigation of a Supersonic Scoop Inlet Derived from a Conical-spike Nose Inlet

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Wittliff, Charles E↗

NASA NTRS1952

Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane I : Two-dimensional Compression-ramp Inlets with Semicircular Cowls

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Valerino, Alfred S↗

NASA NTRS1952

Experimental investigation of axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers : blade-coordinate data

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Lewis, George W , Jr↗

NASA NTRS1952

Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane III : Normal Wedge Inlet with Semicircular Cowl

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Esenwein, Fred T↗