NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience. Volume 1: Summary and analysisThe YF-16 and F-16 developmental wind tunnel test program was reviewed. Geometrical descriptions, general comments, representative data, and the initial efforts toward the development of design guides for the application of strakes to future aircraft are presented.
Document ID
19790019972
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smith, C. W.
(General Dynamics Corp. Fort Worth, TX, United States)
Ralston, J. N.
(General Dynamics Corp. Fort Worth, TX, United States)
Mann, H. W.
(General Dynamics Corp. Fort Worth, TX, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3053
Accession Number
79N28143
Funding Number(s)
CONTRACT_GRANT: NAS1-15006
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available