A Direct Method for Calculation of the Flow About an Axisymmetric Blunt Body at Angle of Attack
1966
42 pages
Report
Keine Angabe
Englisch
Aerodynamics , Angle of attack , Axisymmetric body , Blunt body , Inviscid flow , Supersonic flow , Afterbody , Angle , Attack , Axisymmetry , Blunt , Body , Calculation , Cone , Flight , Flow , Inviscid , Problem , Reentry , Solution , Supersonic