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
A note on the ability to predict transonic drag-rise changes due to model modificationsWind tunnel test to establish validity of Fourier analysis results for transonic drag rise changes due to model modifications
Document ID
19660024789
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Pierpont, P. K. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 3, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L57H07
Report Number: NACA-RM-L57H07
Accession Number
66N34079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FOURIER ANALYSIS
TRANSONIC SPEED
DRAG

Related Records

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