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
Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75 degAerodynamic characteristics in pitch of variable sweep V/STOL configurations tested in supersonic wind tunnel
Document ID
19660011612
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Foster, G. V. (NASA Langley Research Center Hampton, VA, United States)
Morris, O. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-322
Report Number: NASA-TM-X-322
Accession Number
66N20901
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
VARIABLE SWEEP
PITCHING MOMENT
V/STOL AIRCRAFT

Related Records

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