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On the rational design of compressible flow ejectorsA fluid mechanics review of chemical laser ejectors is presented. The characteristics of ejectors with single and multiple driver nozzles are discussed. Methods to compute an optimized performance map in which secondary Mach number and performance are computed versus mass ratio, to compute the flow distortion at each optimized condition, and to determine the thrust area for the design point to match diffuser impedence are examined.
Document ID
19800001875
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ortwerth, P. J.
(Air Force Weapons Lab. Kirtland AFB, NM, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: NASA. Ames Res. Center. Workshop on Thrust Augmenting Ejectors
Subject Category
Aerodynamics
Accession Number
80N10114
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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