Heat-Transfer and Pressure Measurements from a Flight Test of a 1/18-Scale Model of the Titan Intercontinental Ballistic Missile Up to a Mach Number of 3.95 and Reynolds Number Per Foot of 23 by 10 to the 6th Power
| Author: | Graham, John B., Jr. |
|---|---|
| Additional Authors: | Chauvin, Leo T. |
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-SL57L16A |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc53269/ |