Free-Flight Investigation of Effects of Simulated Sonic Turbojet Exhaust on the Drag of Twin-Jet Boattail Bodies at Transonic Speeds

One of 5,157 reports in the series: NACA Research Memorandums available on this site.

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Description

Memorandum presenting a flight investigation to determine the effect of a propulsive jet on the zero-lift drag characteristics of two twin-exit boat-tailed bodies at transonic speeds. The two models had ratios of jet area to base area of 0.394 and 0.590 and covered a Mach number range of 0.8 to 1.15. A slight reduction in drag coefficients from power-off values are obtained during power-on flight for both models.

Physical Description

38 p. : ill.

Creation Information

Leiss, Abraham July 20, 1956.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided by the UNT Libraries Government Documents Department to the UNT Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 20 times. More information about this report can be viewed below.

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  • Main Title: Free-Flight Investigation of Effects of Simulated Sonic Turbojet Exhaust on the Drag of Twin-Jet Boattail Bodies at Transonic Speeds
  • Series Title: NACA Research Memorandums

Description

Memorandum presenting a flight investigation to determine the effect of a propulsive jet on the zero-lift drag characteristics of two twin-exit boat-tailed bodies at transonic speeds. The two models had ratios of jet area to base area of 0.394 and 0.590 and covered a Mach number range of 0.8 to 1.15. A slight reduction in drag coefficients from power-off values are obtained during power-on flight for both models.

Physical Description

38 p. : ill.

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  • Accession or Local Control No: 93R18661
  • URL: http://hdl.handle.net/2060/19930089371 External Link
  • Report No.: NACA-RM-L56D30
  • Center for AeroSpace Information Number: 19930089371
  • Archival Resource Key: ark:/67531/metadc62720

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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).

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Creation Date

  • July 20, 1956

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • Nov. 6, 2018, 2:16 p.m.

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Leiss, Abraham. Free-Flight Investigation of Effects of Simulated Sonic Turbojet Exhaust on the Drag of Twin-Jet Boattail Bodies at Transonic Speeds, report, July 20, 1956; (https://digital.library.unt.edu/ark:/67531/metadc62720/: accessed May 30, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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