Laminar heat transfer distributions for blunted- cone, cone frustum reentry configuration at hypersonic speed using Reynolds number
Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10
01.04.1969
Sonstige
Keine Angabe
Englisch
Spherically blunted cone pressure distributions.
AIAA | 1966
|Spherically Blunted Cone Pressure Distributions
NTIS | 1965
|