A method for shock train leading edge detection based on differential pressure
A method for shock train leading edge detection based on differential pressure
A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INTEGRATED WITH A LONG FOREBODY
The Effect of Sidewall Geometry on Starting Characteristics of Two-dimensional Hypersonic Inlet
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
Optimization of Reentry Trajectory and Overall Parameters of Manned Spacecraft
Nonsilicon micromachining for MOEMS elements [3276-28]