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Results for “Normalization”

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 1,495 records · Page 83

All sources NASA NTRS DOE OSTI

NASA NTRS1954

Investigation of the Normal Force Accompanying Thrust-axis Inclination of the NACA 1.167-(0)(03)-058 and the NACA 1.167-(0)(05)-058 Three-blade Propellers at Forward Mach Numbers to 0.90

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Demele, Fred A↗

NASA NTRS1954

Normal force, center of pressure, and zero lift drag of several ballistic-type missiles at Mach numbers of 4.05

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Ulmann, Edward F↗

NASA NTRS1954

Comparison of experimental and theoretical normal-force distributions (including Reynolds number effects) on an ogive-cylinder body at Mach number 1.98

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Perkins, Edward W↗

NASA NTRS1955

An Experimental Investigation of the Air-flow Stability of a Scoop-type Normal-shock Inlet

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Mossman, Emmet A↗

NASA NTRS1955

The Unsteady Normal-force Characteristics of Selected NACA Profiles at High Subsonic Mach Numbers

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Polentz, Perry P↗

NASA NTRS1956

Investigation of a Continuous Normal-shock Positioning Control on the Bypass of a Supersonic Inlet in Combination with the J34 Turbojet Engine

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Wilcox, Fred A↗

NASA NTRS1955

Effects of Boundary-layer Separation on Normal Force and Center of Pressure of a Cone-cylinder Model with a Large Base Flare at Mach Numbers from 3.00 to 6.28

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Dennis, David H↗

NASA NTRS1953

Rocket-model Investigation to Determine the Hinge-moment and Normal-force Properties of a Full-span, Constant-chord, Partially Balanced Trailing-edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26

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Martz, C William↗

NASA NTRS1956

The Change with Mass-flow Ratio of the Cowl Pressure Drag of Normal-shock Inlets at Supersonic Speeds

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Davis, Wallace F↗

NASA NTRS1956

Transonic-wind-tunnel Investigation of the Effects of Lip Bluntness and Shape on the Drag and Pressure Recovery of a Normal-shock Nose Inlet in a Body of Revolution

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Olstad, Walter B↗

NASA NTRS1956

Dynamic model investigation of two tail-sitter vertically rising airplanes to determine the altitude required to approach normal flight conditions under power failure in hovering flight

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Kliner, Walter J↗

NASA NTRS1957

Investigation of a continuous normal-shock positioning control for a translating-spike supersonic inlet in combination with J34 turbojet engine

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Wilcox, Fred A↗

NASA NTRS1957

Normal-force and Hinge-moment Characteristics at Transonic Speeds of Flap-type Ailerons at Three Spanwise Locations on a 4-percent-thick Sweptback-wing--body Model and Pressure-distribution Measurements on an Inboard Aileron

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Runckel, Jack F↗

NASA NTRS1957

Flight Data Pertinent to Buffeting and Maximum Normal-force Coefficient of the Douglas X-3 Research Airplane

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Baker, Thomas F↗

NASA NTRS1948

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers III : normal-shock diffuser

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Schroeder, Albert H↗

NASA NTRS1958

Wind-tunnel Investigation of the Effects of Lip Geometry on Drag and Pressure Recovery of a Normal-shock Nose Inlet on a Body of Revolution at Mach Numbers of 1.41 and 1.81

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Robins, A Warner↗

NASA NTRS1952

Aeronautical interference effects on normal and axial force coefficients of several engine-strut-body configurations at Mach numbers of 1.8 and 2.0

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Kremzier, Emil J↗

NASA NTRS1954

Experimental Determination of Aerodynamic Forces Normal to the Chord Due to Rotating Stall Acting on Compressor Blading

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Johnson, Donald F↗