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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 1,153 records · Page 64

All sources NASA NTRS DOE OSTI

NASA NTRS1954

Theoretical investigation of longitudinal response characteristics of a swept-wing fighter airplane having a normal acceleration control system and a comparison with other types of systems

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Stokes, Fred H↗

NASA NTRS1956

Calculations of the rate of thermal dissociation of air behind normal shock waves at Mach numbers of 10, 12, and 14

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Wood, George P↗

NASA NTRS1956

Normal component of induced velocity in the vicinity of a lifting rotor with a nonuniform disk loading

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Heyson, Harry H↗

NASA NTRS1956

Distribution of normal component of induced velocity in lateral plane of a lifting rotor

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Castles, Walter, Jr↗

NASA NTRS1956

Method for Calculating Effects of Dissociation on Flow Variables in the Relaxation Zone Behind Normal Shock Waves

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Evans, John, S↗

NASA NTRS1957

Stability of laminar boundary layer near a stagnation point over an impermeable wall and a wall cooled by normal fluid injection

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Morduchow, Morris↗

NASA NTRS1945

Bonding Strengths of Adhesives at Normal and Low Temperatures

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CEMENTS-CYCLEWELD C-3↗

NASA NTRS1958

Tables and Graphs of Normal-shock Parameters at Hypersonic Mach Numbers and Selected Altitudes

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Huber, Paul W↗

NASA NTRS1958

Normal Component of Induced Velocity for Entire Field of a Uniformly Loaded Lifting Rotor with Highly Swept Wake as Determined by Electromagnetic Analog

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Castles, Walter, Jr↗

NASA NTRS1958

Experimental Investigation of Axial and Normal Force Characteristics of Skewed Nozzles

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Carter, David J , Jr↗

NASA NTRS1950

An analysis of the normal accelerations and airspeeds of several Lockheed Constellation L-649 airplanes in postwar commercial transport operations over the eastern part of the United States

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Coleman, Thomas L↗

NASA NTRS1949

Tests of a model horizontal tail of aspect ratio 4.5 in the Ames 12-foot pressure wing tunnel II : elevator hinge line normal to the plane of symmetry

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Tinling, Bruce E↗

NASA NTRS1950

Summary of the first sample of VGH data of normal accelerations and associated operating conditions on two four-engine transport airplanes in commercial operations

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Mcdougal, Robert L↗

NASA NTRS1950

Flight Measurements with the Douglas D-558-II (buaero No. 37974) Research Airplane : Measurements of the Buffet Boundary and Peak Airplane Normal-force Coefficients at Mach Numbers up to 0.90

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Mayer, John P↗

NASA NTRS1950

Summary of normal accelerations, gust velocities, and operating practices, from April to August 1949 of a twin-engine airplane in commercial transport operations

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Steiner, Roy↗

NASA NTRS1951

Tabulated pressure coefficients and aerodynamic characteristics measured in flight on the wing of the Douglas D-558-I airplane throughout the normal-force coefficient range at Mach numbers of 0.67, 0.74, 0.78, and 0.82

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Keener, Earl R↗

NASA NTRS1951

Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the D-558-I Research Airplane Through a Mach Number Range of 0.80 to 0.89 and Throughout the Normal-force-coefficient Range at Mach Numbers of 0.61, 0.7

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Keener, Earl R↗

NASA NTRS1951

Theoretical Investigation of an Automatic Control System with Primary Sensitivity to Normal Accelerations as Used to Control a Supersonic Canard Missile Configuration

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Seaberg, Ernest C↗