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
Similarity laws for lifting wings of minimum drag at hypersonic speedsSimilarity laws for determining chordwise and spanwise contours minimizing drag of flat-top wing in hypersonic flow
Document ID
19660010373
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Miele, A. (Rice Univ. Houston, TX, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
AAR-16
NASA-CR-70729
Report Number: AAR-16
Report Number: NASA-CR-70729
Accession Number
66N19662
Funding Number(s)
CONTRACT_GRANT: NGR-44-006-045
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLOW
FLAT SURFACE
SLENDER WING
MINIMUM DRAG
SIMILARITY HYPOTHESIS

Related Records

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