The problem of thrust increase by air admixture to exhaust jets of rockets, turbojet, ram- and pulse-jet engines is investigated theoretically. The optimum ratio of mixing chamber pressure to ambient pressure and speed range for thrust increase due to air admixture is determined for each type of jet engine.
Air admixture to exhaust jets
1953-07-01
Sonstige
Keine Angabe
Englisch
Noise of Swirling Exhaust Jets
AIAA | 1977
|Noise of swirling exhaust jets
AIAA | 1976
|Photographic Pyrometry of Rocket Exhaust Jets
Emerald Group Publishing | 1959
|Exhaust of Underexpanded Jets from Finite Reservoirs
AIAA | 2010
|Exhaust of Underexpanded Jets from Finite Reservoirs
Online Contents | 2010
|