A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

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Bibliographic Details
Author / Creator:Jackson, Charlie M., author.
Imprint:Washington, D.C. : National Aeronautics and Space Administration, November 1968.
Description:1 online resource (102 pages) : illustrations.
Language:English
Series:NASA technical note ; NASA TN D-4865
NASA technical note ; D-4865.
Subject:
Aerodynamic load.
Noses (Space vehicles) -- Testing.
Angle of attack (Aerodynamics)
Aerodynamics, Supersonic -- Testing.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12674949
Hidden Bibliographic Details
Other authors / contributors:Sawyer, Wallace C., author.
Smith, Rudeen S., author.
United States. National Aeronautics and Space Administration, issuing body.
Notes:"November 1968."
Includes bibliographical references (page 52).
Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 5, 2020).
Other form:Print version: Jackson, Charlie M Method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow
GPO item no.:0830-H-13 (online)
Govt.docs classification:NAS 1.14:D-4865

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