Computer program computes zero lift wave drag of an entire aircraft including any combination of the wing, body, pods, fins, and carnard. The program computes the external volume of the wing and the axial area distribution of the wing equivalent body.
Program computes zero lift wave drag of entire aircraft
1967-12-01
Miscellaneous
No indication
English
Zero-Lift Wave Drag of Complex Aircraft Configurations
NTRS | 1986
|Program Computes Thermodynamic Functions
NTRS | 1994
|Program Computes Thermodynamic Functions
Online Contents | 1994
Program Computes Dendrite-Setting Velocities
Online Contents | 1994
Program Computes Dendrite-Settling Velocities
NTRS | 1994
|