Experimental Investigation of Flow Around Lifting Symmetrical Double-Wedge Airfoils at Mach Numbers of 1.30 and 1.41.
Experimental investigation of flow around lifting symmetrical double-wedge airfoils at mach numbers of 1.30 and 1.41
NACA -- Tech Note
1956
86 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Density fields around sphere at mach numbers 1.30 and 1.62
Engineering Index Backfile | 1950
|Density fields around a sphere at mach numbers 1.30 and 1.62
TIBKAT | 1950
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