NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges
Document ID
19930084017
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Martin, John C
Margolis, Kenneth
Jeffreys, Isabella
Date Acquired
August 16, 2013
Publication Date
June 1, 1952
Report/Patent Number
NACA-TN-2699
Accession Number
93R13307
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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