NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Theoretical investigation for the effects of sweep, leading-edge geometry, and spanwise pressure gradients on transition and wave drag transonic, and supersonic speed with experimental correlations
Document ID
19890040858
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Goradia, S. H. (NASA Langley Research Center Hampton, VA, United States)
Bobbitt, P. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
SAE PAPER 881484
Accession Number
89A28229
Funding Number(s)
CONTRACT_GRANT: NAS1-17919
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

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