30 |
True airspeed in the International Standard Atmosphere and equivalent airspeed corresponding to Mach number and pressure altitude. |
78017 |
30 |
Physical properties of design atmospheres. |
78008 |
30 |
Properties of a Standard atmosphere. |
77021 |
30 |
Reynolds number, speed of sound, dynamic viscosity, kinetic pressure and total pressure coefficient in air. |
73017 |
30 |
Inviscid supersonic flow past cones at zero incidence: (iv) Mach number in the conical flow field. |
70010 |
30 |
Inviscid supersonic flow past cones at zero incidence: (iii) flow deflection in the conical flow field. |
70009 |
30 |
Inviscid supersonic flow past cones at zero incidence: (ii) surface pressure coefficient and shock angle for circular cones. |
AERO S.00.03.13 |
30 |
Inviscid supersonic flow past cones at zero incidence: (i) shock angle. |
70008 |
30 |
Solutions to the Prandtl-Meyer expansion relations for a range of specific heat ratios: pressure coefficient and maximum flow deflection angle. |
AERO 00.03.31 |
30 |
Solutions to the oblique shock wave relations for a range of specific heat ratios: pressure coefficient and detachment angle. |
AERO 00.03.30 |