Flight results showing the effect of mass addition on base pressure

Base pressure results at M equals 4 using free-flight and sting-supported models.

J. M. Cassanto · AIAA Journal · 1968 · 24 citations

Engineering, Aerospace Engineering, Civil Engineering +5

Mean properties of the turbulent near wake of a slender body with and without base injection.

John E. Lewis, Robert L. Chapkis · AIAA Journal · 1969 · 20 citations

Natural Sciences, Aerospace Engineering, Physics +14

Supersonic combustion tests with a double- oblique-shock SCRAMjet ina shock tunnel

I. T. Osgerby, H. K. Smithson, Douglas A. Wagner · AIAA Journal · 1970 · 15 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Local flow effects on base pressure.

J. M. Cassanto, R. S. Mendelson · AIAA Journal · 1968 · 10 citations

Engineering, Petroleum Engineering, Fluid Dynamics +7