A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INTEGRATED WITH A LONG FOREBODY
A method for shock train leading edge detection based on differential pressure
A method for shock train leading edge detection based on differential pressure
Low-threshold, high SMSR tunable external cavity quantum cascade laser around Formula Not Shown
Parametric effects in a scramjet engine on the interaction between the air stream and the injection
Parametric effects in a scramjet engine on the interaction between the air stream and the injection
The Effect of Sidewall Geometry on Starting Characteristics of Two-dimensional Hypersonic Inlet