Design of the nozzle of a jet engineJOSEPH FISCHER,LEERALPH BECKER,EDWARDTHOMAS KUTNEY,JOHNPATRICK MCHUGH,DONALD
Jet engine nozzle for controlling the direction of 优质文献 相似文献 参考文献 引证文献Device for controlling the direction of thrust nozzle of a rocket engine An apparatus for controlling the thrust direction of the supersonic nozzle of the rocket engine of a missile, which in or on from the ...
An improved jet engine two dimensional, asymmetric afterburner nozzle of the type adapted to be mounted on a jet engine suspended from an airfoil's wing sp... A Nozzle,DW Hapke 被引量: 0发表: 2017年 Design and Fabrication of Variable Nozzle for Precooled Turbojet Engine The afterburner an...
combustion chamber and power turbine as shown in Figure 2. However the engine features a second turbine that drives a large fan at the front of the engine. This fan delivers air to a bypass duct that channels air to the exhaust nozzle without passing through a combustion chamber....
For propelling water rockets and jetboats; squirts water out the back through a nozzle【参考译文】对于推动水火箭和喷气快艇来说,它们是通过喷嘴将水从后部喷射出去从而产生推力的。 In boats, can run in shallow water, high acceleration, no risk of engine overload (unlike propellers), less noise an...
engine the flow into the stator and rotor is highly unsteady and of great complexity. However, in a frame of reference fixed to a rotating blade it can be assumed to be fairly steady with sufficient accuracy. For the first row of stators (or nozzle guide vanes) the flow impinges parallel...
Mathematical mode of a turbojet engine with variable geometry exhaust nozzle The engine parameters prognosis is important point in the jet engine and its control system design. The work deals with mathematical modeling mainly focuse... IR Gášpár 被引量: 0发表: 2013年 Aircraft Jet Engine Embe...
not available for EP031552of corresponding document:A thrust reversing system acting on a cold flow air duct of a turbofan-type turbojet engine is disclosed wherein the thrust reversing doors conform to a turbojet engine housing formed as a body revolution about a central longitudinal axis. The...
1. An outer casing 18 is disposed around the engine casing 16 to define therewith an annular passage 19 through which air may flow from the intake 101 to the annular space 20 around the convergent nozzle portion 15, the air then entering into the nozzle by ejector effect of the exhaust ...
A variable area two-stage ejection nozzle exhaust system for a turbojet engine having an afterburner. wherein, a primary nozzle has spherical segments contained within a spherical shell housing which spherical segments are pivotally adjustable in response to augmented and non-augmented engine ...