Effects of Cavity on the Performance of Dual Throat Nozzle During the Thrust-Vectoring Starting Transient Process

Author:

Gu Rui1,Xu Jinglei2

Affiliation:

1. e-mail:

2. Professor at NUAA e-mail:  Department of Power Engineering, Nanjing University of Aeronautics and Astronautics (NUAA), Nanjing 210016, China

Abstract

The dual throat nozzle (DTN) technique is capable to achieve higher thrust-vectoring efficiencies than other fluidic techniques, without compromising thrust efficiency significantly during vectoring operation. The excellent performance of the DTN is mainly due to the concaved cavity. In this paper, two DTNs of different scales have been investigated by unsteady numerical simulations to compare the parameter variations and study the effects of cavity during the vector starting process. The results remind us that during the vector starting process, dynamic loads may be generated, which is a potentially challenging problem for the aircraft trim and control.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference20 articles.

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4. Fluid Thrust-Vector Control of Supersonic Jet Using Coflow Injection;J. Propul. Power,2012

5. Fluidic Throat Skewing for Thrust Vectoring in Fixed-Geometry Nozzles,1999

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