NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
A flat wing with sharp edges in a supersonic streamA basic treatment is given for the approximate solution of the problem of two-dimensional supersonic flow past a thin wing at small angles of attack. The pressure distribution at the surface, the lifting force, and the wave drag are determined.
Document ID
19930093836
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Donov, A E
Date Acquired
August 16, 2013
Publication Date
March 1, 1956
Report/Patent Number
NACA-TM-1394
Report Number: NACA-TM-1394
Accession Number
93R23161
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMICS, FUNDAMENTAL
AERODYNAMICS
FLOW, COMPRESSIBLE
FLOW, SUPERSONIC

Related Records

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