Determination of boundary-layer transition Reynolds numbers by surface-temperature measurement of a 10 [degrees] cone in various NACA supersonic wind tunnels
1953
26 S
graph. Darst
Buch
Englisch
NACA unitary plan wind tunnels
Engineering Index Backfile | 1957
Boundary Layer and Near-Wake Measurements of NACA 0012 Airfoil at Low Reynolds Numbers
British Library Conference Proceedings | 2009
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