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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 109 records · Page 6

All sources NASA NTRS DOE OSTI

NASA NTRS1952

Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane IV : Rectangular Cowl Inlets with Two-dimensional Compression Ramps

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Simon, Paul C↗

NASA NTRS1952

Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane II : Inlets Utilizing Half of a Conical Spike

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Allen, J L↗

NASA NTRS1953

A Flight Comparison of a Submerged Inlet and a Scoop Inlet at Transonic Speeds

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Rolls, L Stewart↗

NASA NTRS1953

Experimental Investigation of an Axial-flow Compressor Inlet Stage Operating at Transonic Relative Inlet Mach Numbers III : Blade-row Performance of Stage with Transonic Rotor and Subsonic Stator at Corrected Tip Speeds of 800 and 1000 Feet Per Secon

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Schwenk, Francis C↗

NASA NTRS1954

Investigation of a 10-stage Subsonic Axial-flow Research Compressor V : Effect of Reducing Inlet-guide-vane Turning on Over-all and Inlet-stage Performance

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Budinger, Ray E↗

NASA NTRS1953

Experimental Investigation of a 0.4 Hub-tip Diameter Ratio Axial-flow Compressor Inlet Stage at Transonic Inlet Relative Mach Numbers I : Rotor Design and Over-all Performance at Tip Speeds from 60 to 100 Percent of Design

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Serovy, George K↗

NASA NTRS1957

Performance Evaluation of Reduced-chord Rotor Blading as Applied to J73 Two-stage Turbine V : Effect of Inlet Pressure on Over-all Performance at Design Speed and Inlet Temperature of 700 R

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Schum, Harold J↗

NASA NTRS1954

Some internal-flow characteristics at zero flight speed of an annular supersonic inlet and an open-nose inlet with sharp and rounded lips

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Milillo, Joseph R↗

NASA NTRS1954

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↗

NASA NTRS1954

Experimental Investigation of an Axial-flow Compressor Inlet Stage Operating at Transonic Relative Inlet Mach Numbers IV : Stage and Blade-row Performance of Stage with Axial-discharge Stators

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Sandercock, Donald M↗

NASA NTRS1955

Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers II : stage and blade-element performance

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Montgomery, John C↗

NASA NTRS1955

Inlet-air Distortion Effects on Stall, Surge, and Acceleration Margin of a Turbojet Engine Equipped with Variable Compressor Inlet Guide Vanes

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Harry, David P , III↗

NASA NTRS1956

Fuselage Side Inlets : a Study of Some Factors Affecting Their Performance and a Comparison with Nose Inlets

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Mossman, Emmet A↗

NASA NTRS1956

Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers III : effect of tip taper on over-all and blade-element performances

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Montgomery, John C↗

NASA NTRS1956

Investigation at Transonic Speeds of the Effects of Inlet Lip Stagger on the Internal-flow Characteristics of an Unswept Semielliptical Air Inlet

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Bingham, Gene J↗

NASA NTRS1956

Experimental Investigation of a Transonic Axial-flow-compressor Rotor Designed for Sonic Inlet Velocity with an Inlet Hub-tip Radius Ratio of 0.35

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Boxer, Emanuel↗

NASA NTRS1956

Performance of Supersonic Ramp-type Side Inlet with Combinations of Fuselage and Inlet Throat Boundary-layer Removal

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Campbell, Robert C↗

NASA NTRS1957

Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers IV : performance of tapered-tip rotor configuration with reset blade angles

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Montgomery, John C↗