Base pressure distribution of two blunted cones at Mach numbers from 0.3 to 0.8 and 1.81 to 3.51
Base pressure distribution on blunted cones during supersonic wind tunnel tests
Kerr, W. R.↗
Engineering topics
Publications and source records attributed to Kerr, W. R..
Base pressure distribution on blunted cones during supersonic wind tunnel tests
Hypersonic wind tunnel stagnation conditions, wedge flow measurements, transonic entry capsule configuration, and internal pressure in conical pintle nozzle