Effect of circumferential location on angle of attack performance of twin half-conical scoop-type inlets mounted symmetrically on the RM-10 body of revolution

One of 5,163 reports in the series: NACA Research Memorandums available on this site.

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Description

Report presenting an investigation to determine the effect of circumstantial inlet location on the performance of twin half-conical scoop-type inlets with and without boundary-layer removal at several Mach numbers and angles of attack. For positive angles of attack, higher pressure recovery performance was obtained with the inlets mounted on lower fuselage quadrants than on upper quadrants.

Physical Description

37 p. : ill.

Creation Information

Valerino, Alfred S.; Pennington, Donald B. & Vargo, Donald J. September 9, 1953.

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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 48 times . More information about this report can be viewed below.

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  • Main Title: Effect of circumferential location on angle of attack performance of twin half-conical scoop-type inlets mounted symmetrically on the RM-10 body of revolution
  • Series Title: NACA Research Memorandums

Description

Report presenting an investigation to determine the effect of circumstantial inlet location on the performance of twin half-conical scoop-type inlets with and without boundary-layer removal at several Mach numbers and angles of attack. For positive angles of attack, higher pressure recovery performance was obtained with the inlets mounted on lower fuselage quadrants than on upper quadrants.

Physical Description

37 p. : ill.

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  • Accession or Local Control No: 93R16887
  • URL: http://hdl.handle.net/2060/19930087597 External Link
  • Report No.: NACA-RM-E53G09
  • Center for AeroSpace Information Number: 19930087597
  • Archival Resource Key: ark:/67531/metadc59616

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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

  • September 9, 1953

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • April 3, 2018, 1:21 p.m.

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Valerino, Alfred S.; Pennington, Donald B. & Vargo, Donald J. Effect of circumferential location on angle of attack performance of twin half-conical scoop-type inlets mounted symmetrically on the RM-10 body of revolution, report, September 9, 1953; (digital.library.unt.edu/ark:/67531/metadc59616/: accessed August 14, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.