NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Charts for the Determination of Supersonic Air Flow Against Inclined Planes and Axially Symmetric Cones
Document ID
19930082009
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moeckel, W E
Connors, J F
Date Acquired
August 16, 2013
Publication Date
July 1, 1947
Report/Patent Number
NACA-TN-1373
Report Number: NACA-TN-1373
Accession Number
93R11299
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR FLOW - SHOCK WAVES
AIR FLOW - CONES
CHARTS - AIR FLOW
AIR FLOW - AIRFOILS, WEDGE
EQUATIONS - SHOCK WAVES
AIR FLOW VELOCITY, HIGH-SUPERSONIC
AIR FLOW - CORNERS
No Preview Available