Internal Performance Characteristics of Vectored Axisymmetric Ejector Nozzles

Internal Performance Characteristics of Vectored Axisymmetric Ejector Nozzles PDF Author: Milton Lamb
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Category :
Languages : en
Pages :

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Internal Performance Characteristics of Vectored Axisymmetric Ejector Nozzles

Internal Performance Characteristics of Vectored Axisymmetric Ejector Nozzles PDF Author: Milton Lamb
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Category :
Languages : en
Pages :

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Internal Performance Characteristics of Thrust-vectored Axisymmetric Ejector Nozzles

Internal Performance Characteristics of Thrust-vectored Axisymmetric Ejector Nozzles PDF Author: Milton Lamb
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Category :
Languages : en
Pages : 232

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Internal Performance Characteristics of Thrust-Vectored Axisymmetric Ejector Nozzles

Internal Performance Characteristics of Thrust-Vectored Axisymmetric Ejector Nozzles PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724261922
Category :
Languages : en
Pages : 232

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A series of thrust-vectored axisymmetric ejector nozzles were designed and experimentally tested for internal performance and pumping characteristics at the Langley research center. This study indicated that discontinuities in the performance occurred at low primary nozzle pressure ratios and that these discontinuities were mitigated by decreasing expansion area ratio. The addition of secondary flow increased the performance of the nozzles. The mid-to-high range of secondary flow provided the most overall improvements, and the greatest improvements were seen for the largest ejector area ratio. Thrust vectoring the ejector nozzles caused a reduction in performance and discharge coefficient. With or without secondary flow, the vectored ejector nozzles produced thrust vector angles that were equivalent to or greater than the geometric turning angle. With or without secondary flow, spacing ratio (ejector passage symmetry) had little effect on performance (gross thrust ratio), discharge coefficient, or thrust vector angle. For the unvectored ejectors, a small amount of secondary flow was sufficient to reduce the pressure levels on the shroud to provide cooling, but for the vectored ejector nozzles, a larger amount of secondary air was required to reduce the pressure levels to provide cooling. Lamb, Milton Langley Research Center NASA-TM-4610, L-17386, NAS 1.15:4610 RTOP 505-59-30-04...

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
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Category : Aeronautics
Languages : en
Pages : 704

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Static Internal Performance Characteristics of Two Thrust-reverser Concepts for Axisymmetric Nozzles

Static Internal Performance Characteristics of Two Thrust-reverser Concepts for Axisymmetric Nozzles PDF Author: Laurence D. Leavitt
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 28

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
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Category : Aeronautics
Languages : en
Pages : 176

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Static Internal Performance of an Axisymmetric Nozzle with Multiaxis Thrust-vectoring Capability

Static Internal Performance of an Axisymmetric Nozzle with Multiaxis Thrust-vectoring Capability PDF Author: George T. Carson
Publisher:
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Category : Airplanes
Languages : en
Pages : 84

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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Category : Government publications
Languages : en
Pages : 1282

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
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Category : Government publications
Languages : en
Pages : 1638

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Static Internal Performance Characteristics of Two Thrust-reverser Concepts for Axisymmetric Nozzles

Static Internal Performance Characteristics of Two Thrust-reverser Concepts for Axisymmetric Nozzles PDF Author: Laurence D. Leavitt
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 28

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