Investigation of the propulsive characteristics of a helicopter-type pulse-jet engine over a range of Mach numbers and angle of yaw

One of 4,119 reports in the series: NACA Technical Notes available on this site.

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Description

Report presenting a determination of the nonwhirling propulsive characteristics of a helicopter-type pulse-jet engine mounted on a simulated helicopter rotor blade in the 16-foot transonic tunnel. Propulsive characteristics as a function of fuel-flow rate at a variety of Mach numbers and angles of yaw. Results regarding engine propulsive characteristics, comparison of whirling and nonwhirling data, and effect of engine operation on airfoil surface pressures are provided.

Physical Description

24 p. : ill.

Creation Information

Carpenter, Paul J.; Shivers, James P. & Lee, Edwin E., Jr. January 1956.

Context

This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and one other and was provided by UNT Libraries Government Documents Department to Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 409 times , with 11 in the last month . More information about this report can be viewed below.

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  • Main Title: Investigation of the propulsive characteristics of a helicopter-type pulse-jet engine over a range of Mach numbers and angle of yaw
  • Series Title: NACA Technical Notes

Description

Report presenting a determination of the nonwhirling propulsive characteristics of a helicopter-type pulse-jet engine mounted on a simulated helicopter rotor blade in the 16-foot transonic tunnel. Propulsive characteristics as a function of fuel-flow rate at a variety of Mach numbers and angles of yaw. Results regarding engine propulsive characteristics, comparison of whirling and nonwhirling data, and effect of engine operation on airfoil surface pressures are provided.

Physical Description

24 p. : ill.

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Identifier

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  • Accession or Local Control No: 93R13659
  • URL: http://hdl.handle.net/2060/19930084369 External Link
  • Report No.: NACA-TN-3625
  • Center for AeroSpace Information Number: 19930084369
  • Archival Resource Key: ark:/67531/metadc57888

Collections

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National Advisory Committee for Aeronautics Collection

The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915 to undertake, promote, and institutionalize aeronautical research. On October 1, 1958 the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA).

Technical Report Archive and Image Library

This selection of materials from the Technical Report Archive and Image Library (TRAIL) includes hard-to-find reports published by various government agencies. The technical publications contain reports, images, and technical descriptions of research performed for U.S. government agencies. Topics range from mining, desalination, and radiation to broader physics, biology, and chemistry studies. Some reports include maps, foldouts, blueprints, and other oversize materials.

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Creation Date

  • January 1956

Added to The UNT Digital Library

  • Nov. 16, 2011, 7:33 a.m.

Description Last Updated

  • April 10, 2018, 2:44 p.m.

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Carpenter, Paul J.; Shivers, James P. & Lee, Edwin E., Jr. Investigation of the propulsive characteristics of a helicopter-type pulse-jet engine over a range of Mach numbers and angle of yaw, report, January 1956; (digital.library.unt.edu/ark:/67531/metadc57888/: accessed November 12, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.