Aerothermal Analysis for Configuration Design of Swept Leading Edge Hypersonic Vehicle
Aerothermal Analysis for Configuration Design of Swept Leading Edge Hypersonic Vehicle
Long wave infrared signature of swept back leading edges in aircraft frontal aspect
Infrared Signature of Fixed and Variable Area C-D Nozzle of Aircraft Engine
Analysis of Infrared Signature from Aircraft Frontal Aspect due to Skin Friction Heating