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.
Series InformationTechnical note (United States. National Advisory Committee for Aeronautics) ; 2711.
- Physical Description: 1 online resource (30 pages) : illustrations.
- Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 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).
Search for related items by subject
|Subject:||Nozzles > Fluid dynamics.
Supersonic nozzles > Design and construction.
Wind tunnel testing.