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The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / by Ivan E. Beckwith, Herbert W. Ridyard, and Nancy Cromer.

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Record details

  • Physical Description: 1 online resource (30 pages) : illustrations.
  • Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1952.

Content descriptions

General Note:
"June 1952."
No Federal Depository Library Program (FDLP) item number.
Bibliography, etc. Note:
Includes bibliographical references (page 18).
Source of Description Note:
Description based on online resource, PDF version; title from title page (TRAIL, viewed July 21, 2020).
Subject: Nozzles > Fluid dynamics.
Supersonic nozzles > Design and construction.
Axial flow.
Wind tunnel testing.
Mathematical analysis.

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