A unified approach to the problem of gaseous jet penetration into a supersonic stream
Unified model for transverse gaseous jet penetration into supersonic stream agreeing with measured flow field properties
Billig, F. S.↗
Engineering topics
Publications and source records attributed to Lasky, M..
Unified model for transverse gaseous jet penetration into supersonic stream agreeing with measured flow field properties
Thermal compression effects on hypersonic ramjets performance, discussing thermodynamic cycle calculation based on gas dynamic model
Two-dimensional turbulent mixing scaling laws of mixing, heat transfer and skin friction for use in design of scramjet engine combustors