NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
First-order theory for unsteady motion of thin wings at supersonic speeds
Document ID
19930082691
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moskowitz, Barry
Moeckel, W E
Date Acquired
August 16, 2013
Publication Date
February 1, 1950
Report/Patent Number
NACA-TN-2034
Report Number: NACA-TN-2034
Accession Number
93R11981
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER - WINGS
PRESSURE DISTRIBUTION - WINGS
LOAD DISTRIBUTION, WING-SPAN
WIGNS - OSCILLATIONS
WINGS, THIN
THEORIES - WINGS SUPERSONIC
No Preview Available