NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
INVESTIGATION OF BOUNDARY LAYER PARAMETERS IN APG NOZZLE AND THE FLOW INTERFERENCE CAUSED BY SECONDARY INJECTIONFlow interference caused by secondary injection in adverse pressure gradient nozzles - boundary layer parameter investigations
Document ID
19630010059
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gagnon, R. (National Engineering Science Co. Pasadena, CA, United States)
Hozaki, S. (National Engineering Science Co. Pasadena, CA, United States)
Mayer, E. (National Engineering Science Co. Pasadena, CA, United States)
Tromblay, J. (National Engineering Science Co. Pasadena, CA, United States)
Wu, J. (National Engineering Science Co. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1963
Subject Category
Aircraft
Report/Patent Number
SN-101
NASA-CR-50606
Report Number: SN-101
Report Number: NASA-CR-50606
Accession Number
63N19939
Funding Number(s)
CONTRACT_GRANT: NAS7-166
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GAS FLOW
INTERFERENCE
SECONDARY INJECTION
PRESSURE GRADIENT
BOUNDARY LAYER SEPARATION
NOZZLE

Related Records

There are no records associated with this record.
No Preview Available