Steady flow about curved airfoils is investigated analytically, first assuming air behaves as an ideal gas, and then assuming it behaves as a thermally perfect, calorically imperfect gas. Conclusions are drawn from the study.
A study of inviscid flow about airfoils at high supersonic speeds
01.01.1953
Sonstige
Keine Angabe
Englisch
Inviscid flow about airfoils at high supersonic speeds
Engineering Index Backfile | 1952
|Inviscid flow about airfoils at high supersonic speeds
TIBKAT | 1952
|Inviscid flow about airfoils at high supersonic speeds
NTRS | 1952
|Study of inviscid flow about airfoils at high supersonic speeds
Engineering Index Backfile | 1953
|