Unsteady Pressure Loads in a Generic High Speed Engine Model

Unsteady Pressure Loads in a Generic High Speed Engine Model PDF Author: Tony L. Parrott
Publisher:
ISBN:
Category : Noise control
Languages : en
Pages : 84

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Unsteady Pressure Loads in a Generic High Speed Engine Model

Unsteady Pressure Loads in a Generic High Speed Engine Model PDF Author: Tony L. Parrott
Publisher:
ISBN:
Category : Noise control
Languages : en
Pages : 84

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702

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Unsteady Pressure Loads in a Generic High Speed Engine Model

Unsteady Pressure Loads in a Generic High Speed Engine Model PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722853969
Category :
Languages : en
Pages : 82

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Unsteady pressure loads were measured along the top interior wall of a generic high-speed engine (GHSE) model undergoing performance tests in the combustion-Heated Scramjet Test Facility at the Langley Research Center. Flow to the model inlet was simulated at 72000 ft and a flight Mach number of 4. The inlet Mach number was 3.5 with a total temperature and pressure of 1640 R and 92 psia. The unsteady pressure loads were measured with 5 piezoresistive gages, recessed into the wall 4 to 12 gage diameters to reduce incident heat flux to the diaphragms, and distributed from the inlet to the combustor. Contributors to the unsteady pressure loads included boundary layer turbulence, combustion noise, and transients generated by unstart loads. Typical turbulent boundary layer rms pressures in the inlet ranged from 133 dB in the inlet to 181 dB in the combustor over the frequency range from 0 to 5 kHz. Downstream of the inlet exist, combustion noise was shown to dominate boundary layer turbulence noise at increased heat release rates. Noise levels in the isolator section increased by 15 dB when the fuel-air ratio was increased from 0.37 to 0.57 of the stoichiometric ratio. Transient pressure disturbances associated with engine unstarts were measured in the inlet and have an upstream propagation speed of about 7 ft/sec and pressure jumps of at least 3 psia. Parrott, Tony L. and Jones, Michael G. and Thurlow, Ernie M. Langley Research Center...

NASA Tech Briefs

NASA Tech Briefs PDF Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1454

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 720

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February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index

Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1786

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Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 300)

Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 300) PDF Author:
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ISBN:
Category :
Languages : en
Pages : 686

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Journal of Propulsion and Power

Journal of Propulsion and Power PDF Author:
Publisher:
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Category : Rocketry
Languages : en
Pages : 822

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Index to ... NASA Tech Briefs

Index to ... NASA Tech Briefs PDF Author:
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Category : NASA tech briefs
Languages : en
Pages : 180

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The Aeronautical Journal

The Aeronautical Journal PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 820

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