A procedure that allows rapid preliminary evaluations of the vertical, short, and normal takeoff performance of supersonic cruise aircraft concepts was developed into a numerical computer program. The program is used to determine the effects on takeoff performance of various parameters, such as thrust-weight ratio, wing loading, thrust vector angle, and flap setting. Ramp-assisted takeoffs for overloaded configurations typical of a ground-attack mission are included. The effects of wind on the takeoff performance are also considered.
Calculation of Vertical and Ramp-Assisted Takeoffs for Supersonic Cruise Fighters
1984
32 pages
Report
No indication
English
Short Takeoffs for Jet Aircraft
NTIS | 1969
|Jet Transport Rejected Takeoffs
NTIS | 1977
|British Library Online Contents | 2005
|Online Contents | 1998
|