20 |
Conditions behind normal shock waves in a perfect gas for various values of gamma. |
AERO 00.03.28 |
20 |
Conditions behind oblique shock waves for air in dissociation equilibrium. |
AERO S.00.03.23 |
20 |
Conditions behind normal shock waves in air in dissociation equilibrium. |
AERO S.00.03.22 |
20 |
Conditions for shock wave detachment and for subsonic flow behind nose shock waves on cones at zero incidence and on wedges. |
AERO S.00.03.16 |
20 |
Pitot and static tubes in supersonic flow. |
AERO S.00.03.15 |
20 |
Approximate calculation of the pressure changes in two-dimensional supersonic flow. |
AERO S.00.03.14 |
20 |
Properties of plane steady shock waves. |
AERO S.00.03.09 |
20 |
Simple-wave flow. |
AERO S.00.03.08 |
20 |
Introductory sheet on isentropic flow and shock waves. |
AERO S.00.03.06 |
20 |
Isentropic expansion of air from rest. |
AERO 00.03.05 |