Flow processes in overexpanded chemical rocket nozzles. Part 2, Side loads due to asymmetric separation /

Bibliographic Details
Main Author:	Schmucker, Robert H.
Corporate Author:	United States. National Aeronautics and Space Administration
Format:	Government Document Microform Book
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, [1984]
Series:	NASA technical memorandum ; 77395.
Subjects:	Rockets (Aeronautics) > Nozzles. Loads (Forces) Pressure distribution. Rocket nozzles. Separated flow. Space shuttle main engine.
Online Access:	https://purl.fdlp.gov/GPO/LPS98675

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