Effect of Free-stream Mach Number on Gross-force and Pumping Characteristics of Several Ejectors PDF Download

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Effect of Free-stream Mach Number on Gross-force and Pumping Characteristics of Several Ejectors

Effect of Free-stream Mach Number on Gross-force and Pumping Characteristics of Several Ejectors PDF Author: Leonard E. Stitt
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ISBN:
Category : Aeronautics
Languages : en
Pages : 42

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Effect of Free-stream Mach Number on Gross-force and Pumping Characteristics of Several Ejectors

Effect of Free-stream Mach Number on Gross-force and Pumping Characteristics of Several Ejectors PDF Author: Leonard E. Stitt
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 42

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Characteristics of Five Ejector Configurations at Free-stream Mach Numbers from 0 to 2.0

Characteristics of Five Ejector Configurations at Free-stream Mach Numbers from 0 to 2.0 PDF Author: John L. Klann
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ISBN:
Category : Ejector pumps
Languages : en
Pages : 46

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 104

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Effect of Afterbody Ejection Configurations on the Performance at Transonic Speeds of a Pylon-supported Nacelle Model Having a Hot-jet Exhaust

Effect of Afterbody Ejection Configurations on the Performance at Transonic Speeds of a Pylon-supported Nacelle Model Having a Hot-jet Exhaust PDF Author: John M. Swihart
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Category : Propulsion systems
Languages : en
Pages : 60

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Investigation at Supersonic and Subsonic Mach Numbers of Auxiliary Inlets Supplying Secondary Air Flow to Ejector Exhaust Nozzles

Investigation at Supersonic and Subsonic Mach Numbers of Auxiliary Inlets Supplying Secondary Air Flow to Ejector Exhaust Nozzles PDF Author: Donald P. Hearth
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 52

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The results indicated increases in auxiliary-inlet pressure recovery with increases in scoop height relative to the boundary-layer thickness. The pressure recovery increased at about the same rate as theoretically predicted for an inlet in a boundary layer having a one-seventh power profile, but was only about 0.68 to 0.75 of the theoretically obtainable values. Under some operating conditions, flow from the primary jet was exhausted through the auxiliary inlet. This phenomenon could be predicted from the ejector pumping characteristics.

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 860

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Index of N A S A Technical Publications

Index of N A S A Technical Publications PDF Author: United States. National Aeronautics and Space Administration
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Category :
Languages : en
Pages : 210

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 218

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Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 494

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Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 208

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