Viscous shock layer flow in the windward plane of cones at angle of attack

This publication has 2 references indexed in Scilit:

• Hypersonic boundary layer studies on a spinning sharp cone at angle of attack
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1971
• CHEMICALLY REACTING VISCOUS FLOW PROGRAM FOR MULTI-COMPONENT GAS MIXTURES.
  Published by Office of Scientific and Technical Information (OSTI) ,1971