Propellant Vaporization as a Design Criterion for Rocket-engine Combustion Chambers PDF Download
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Author: Richard J. Priem
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 64
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Author: Richard J. Priem
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 64
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Author: Marcus F. Heidmann
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1274
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Author: Donald F. Johnson
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 672
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Book Description
Comparison in bending and torsional deflection tests showed thermenol to have a modulus of elasticity of about 26,000,000 and a modulus of rigidity of abot 9,000,000.
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
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Author:
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ISBN:
Category : Patents
Languages : en
Pages : 800
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Author: Robert C. Kohl
Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 728
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A double set of turning vanes was carried inside the jet tailpipe. To produce reverse thrust, the tailpipe opens into two side sections and the turning vanes move outward to form a V-shaped cascade, which deflects the exhaust-gas flow. Forward and reverse net thrust were measured over a range of engine speeds with the airplane stationary. Taxi tests were made to determine the comparative stopping distances using wheel braking and reverse thrust separately, and a combination of both. The effect of turning-vane spacing on thrust-reverser performance was determined by scale-model tests using unheated air.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 546
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Author:
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ISBN:
Category : Metabolism
Languages : en
Pages : 576
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Author: Richard J. Priem
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 68
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