The Effects of a Small Jet of Air Exhausting From the Nose of a Body of Revolution in Supersonic Flow Metadata
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- Main Title The Effects of a Small Jet of Air Exhausting From the Nose of a Body of Revolution in Supersonic Flow
- Series Title NACA Research Memorandums
Author: Love, Eugene S.Creator Type: Personal
Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
- Creation: 1952-11-12
- Content Description: Report presenting the results of an investigation to determine the effects of a small jet of air exhausting from the nose of an elliptical body of revolution upon boundary-layer transition and the viscous, pressure, and total drag of the forebody at three body stations at Mach number 1.62. The jet effects on body pressure, pressure variations, boundary-layer transition, and total drag are provided.
- Physical Description: 45 p. : ill.
- Keyword: aerodynamics
- Keyword: body pressure
Name: National Advisory Committee for Aeronautics CollectionCode: NACA
Name: Technical Report Archive and Image LibraryCode: TRAIL
Name: UNT Libraries Government Documents DepartmentCode: UNTGD
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
- Accession or Local Control No: 93R16648
- URL: http://hdl.handle.net/2060/19930087358
- Report No.: NACA-RM-L52I19a
- Center for AeroSpace Information Number: 19930087358
- Archival Resource Key: ark:/67531/metadc279634