NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
The flexible rectangular wing in roll at supersonic flight speeds
Document ID
19930082442
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Tucker, Warren A
Nelson, Robert L
Date Acquired
August 16, 2013
Publication Date
December 1, 1948
Report/Patent Number
NACA-TN-1769
Report Number: NACA-TN-1769
Accession Number
93R11732
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR FLOW VELOCITY, HIGH - SUPERSONIC
WINGS, RECTANGULAR
ROLLING MOMENTS
WINGS - AEROELASTICITY
STABILITY & CONTROL, LATERAL
WINGS - TORSION
No Preview Available