NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Charts for Conical and Two-Dimensional Oblique-Shock Flow Parameters in Helium at Mach Numbers from About 1 to 100Charts are presented for the determination of certain flow properties in the flow properties in the flow field and on the surface of cones and wedges at Mach numbers from about 1 to 100 in a perfect gas wigh a ratio of specific heats of 5/3. In addition, a table of the isentropic subsonic flow parameters is included.
Document ID
20040006346
Acquisition Source
Langley Research Center
Document Type
Other - NASA Technical Note (TN)
Authors
Arthur Henderson, Jr
(Langley Research Center Hampton, Virginia, United States)
Dorothy 0 Braswel
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 21, 2013
Publication Date
June 1, 1961
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
L-244
NASA-TN-D-819
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available