Comparison of the experimental and theoretical distribution of lift on a slender inclined body of revolution at M = 2 Metadata
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Title
- Main Title Comparison of the experimental and theoretical distribution of lift on a slender inclined body of revolution at M = 2
- Series Title NACA Research Memorandums
Creator
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Author: Perkins, Edward W.Creator Type: Personal
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Author: Kuehn, Donald M.Creator Type: Personal
Contributor
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Originator: Ames Aeronautical Laboratory (U.S.)Contributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Ames Aeronautical Lab
Date
- Creation: 1953-08-25
Language
- English
Description
- Content Description: From Summary: "Pressure distributions and force characteristics have been determined for a body of revolution consisting of a fineness ratio 5.75, circular-arc, ogival nose tangent to a cylindrical afterbody for an angle-of-attack range of 0 degrees to 35.5 degrees. The free-stream Mach number was 1.98 and the free-stream Reynolds number was approximately 0.5 x 10 sup 6, based on body diameter. Comparison of the theoretical and experimental pressure distributions shows that for zero lift, either slender-body theory or higher-order theories yield results which are in good agreement with experiment."
- Physical Description: 39 p. : ill.
Subject
- Keyword: lift characteristics
- Keyword: flow characteristics
- Keyword: aerodynamics
Collection
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Name: National Advisory Committee for Aeronautics CollectionCode: NACA
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Name: Technical Report Archive and Image LibraryCode: TRAIL
Institution
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Name: UNT Libraries Government Documents DepartmentCode: UNTGD
Rights
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
Resource Type
- Report
Format
- Text
Identifier
- Accession or Local Control No: 93R16834
- URL: http://hdl.handle.net/2060/19930087544
- Report No.: NACA-RM-A53E01
- Center for AeroSpace Information Number: 19930087544
- Archival Resource Key: ark:/67531/metadc59580