Summary of available theoretical and experimental investigations made to study shock waves generated by aircraft at supersonic speed and propagation through nonhomogeneous atmosphere; appreciable pressure disturbances can be imposed on ground as result of shock waves extending to ground level; means of reducing shock-wave intensity at ground level; effect on operation of other aircraft in vicinity.
Some aspects of shock-wave generation by supersonic airplanes
AGARD -- Report
1959
19 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Thrust Requirements for Supersonic Airplanes
NTIS | 1960
|Optimal cruise trajectories for supersonic airplanes
TIBKAT | 1972
|Optimal cruise trajectories for supersonic airplanes
NTRS | 1972
|Fuel balance system for supersonic airplanes
Engineering Index Backfile | 1956
|