NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Prediction of heat-transfer characteristics for ejector exhaust nozzlesHeat balance equation for predicting heat transfer of ejector exhaust nozzle at afterburning phase
Document ID
19700012072
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Chenweth, F. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Lieberman, A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Publication Information
Publication: L. METHODS IN AIRCRAFT AERODYN. 1970
Subject Category
Thermodynamics And Combustion
Accession Number
70N21377
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available