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Results for “Power modeling”

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 55 records · Page 3

All sources NASA NTRS DOE OSTI

NASA NTRS1954

An Investigation of the Use of Rocket-powered Models for Gust-load Studies with an Application to a Tailless Swept-wing Model at Transonic Speeds

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LOADS AND STRESSES, STRUCTURAL - DYNAMIC↗

NASA NTRS1957

A limited correlation of atmospheric sounding data and turbulence experienced by rocket-powered models

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Mason, Homer P↗

NASA NTRS1957

A collection of data for zero-lift damping in roll of wing-body combinations as determined with rocket-powered models equipped with roll-torque nozzles

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Stone, David G↗

NASA NTRS1948

Tank Spray Tests of a Jet-powered Model Fitted with NACA Hydro-skis

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Wadlin, Kenneth L↗

NASA NTRS1949

A Free-flight Technique for Measuring Damping in Roll by Use of Rocket-powered Models and Some Initial Results for Rectangular Wings

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Edmondson, James L↗

NASA NTRS1950

Wing-dropping characteristics of some straight and swept wings at transonic speeds as determined with rocket-powered models

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Stone, David G↗

NASA NTRS1950

Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40 degree sweepback

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D'Aiutolo, Charles T↗

NASA NTRS1951

Preliminary Investigation of a Fin-actuated Jet-vane Control System for Stabilization of Rocket-powered Models

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Wineman, Andrew R↗

NASA NTRS1951

Some recent data from flight tests of rocket-powered models

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Source record↗

NASA NTRS1951

Damping in roll of straight and 45 degree swept wings of various taper ratios determined at high subsonic, transonic, and supersonic speeds with rocket-powered models

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Sanders, E Claude, Jr↗

NASA NTRS1951

Flight Determination of the Drag and Longitudinal Stability and Control Characteristics of a Rocket-powered Model of a 60 Degrees Delta-wing Airplane from Mach Numbers 0.75 to 1.70

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Mitcham, Grady L↗

NASA NTRS1952

Use of an Aerodynamically Pulsed All-movable Horizontal Tail to Obtain Longitudinal Characteristics of Rocket-powered Models in Free Flight and Some Initial Results from an Arrow-wing-body-tail Configuration

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Gillespie, Warren, Jr↗

NASA NTRS1952

Some Effects of Body Cross-sectional Shape, Including Sunken-canopy Design, on Drag as Shown by Rocket-powered-model Tests at Mach Numbers from 0.8 to 1.5

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Stoney, William E , Jr↗

NASA NTRS1953

A collection of data for zero-lift damping in roll of wing-body combinations as determined with rocket-powered models equipped with roll-torque nozzles

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Stone, David G↗

NASA NTRS1952

Summary of Some Effective Aerodynamic Twisting-moment Coefficients of Various Wing-control Configurations at Mach Numbers from 0.6 to 1.7 as Determined from Rocket-powered Models

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Strass, H Kurt↗

NASA NTRS1954

Rocket-powered Model Investigation of Lift, Drag, and Stability of a Body-tail Configuration at Mach Numbers from 0.8 to 2.3 and Angles of Attack Between plus or Minus 6.5 Degrees

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Gillespie, Warren, Jr↗

NASA NTRS1954

Rocket-powered-model Investigation of the Hinge-moment and Normal-force Characteristics of a Half-diamond Tip Control on a 60 Degree Sweptback Diamond Wing Between Mach Numbers of 0.5 and 1.3

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Church, James D↗

NASA NTRS1954

Transonic Flight Test of a Rocket-powered Model to Determine Propulsive Jet Influence on the Configuration Drag

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Demoraes, Carlos, A↗