An Oil Flow Study of a Sonic Reaction Jet Ejecting from a Body of Revolution Into a Free Stream of Mach Number Range 1.75 to 4.5 PDF Download

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An Oil Flow Study of a Sonic Reaction Jet Ejecting from a Body of Revolution Into a Free Stream of Mach Number Range 1.75 to 4.5

An Oil Flow Study of a Sonic Reaction Jet Ejecting from a Body of Revolution Into a Free Stream of Mach Number Range 1.75 to 4.5 PDF Author: Troy A. Street
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 696

Book Description
An oil flow test was conducted to obtain flow patterns in the vicinity of a transverse sonic jet ejecting from a body of revolution into an oncoming supersonic flow of M = 1.75, 2.0, 3.0, 4.0, and 4.5. The angle of attack was plus or minus 10 degrees with jet total-to-free stream static pressure ratios up to 100. The jet was oriented to various angular positions at several longitudinal body locations. (Author).

An Oil Flow Study of a Sonic Reaction Jet Ejecting from a Body of Revolution Into a Free Stream of Mach Number Range 1.75 to 4.5

An Oil Flow Study of a Sonic Reaction Jet Ejecting from a Body of Revolution Into a Free Stream of Mach Number Range 1.75 to 4.5 PDF Author: Troy A. Street
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 696

Book Description
An oil flow test was conducted to obtain flow patterns in the vicinity of a transverse sonic jet ejecting from a body of revolution into an oncoming supersonic flow of M = 1.75, 2.0, 3.0, 4.0, and 4.5. The angle of attack was plus or minus 10 degrees with jet total-to-free stream static pressure ratios up to 100. The jet was oriented to various angular positions at several longitudinal body locations. (Author).

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ISBN:
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