Numerical investigation of lateral jet interaction effects on the hypersonic quasi-waverider vehicle-Reference-Cited by-同舟云学术

Numerical investigation of lateral jet interaction effects on the hypersonic quasi-waverider vehicle

Published:2015-05-19 Issue:14 Volume:229 Page:2671-2680
ISSN:0954-4100
Container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Author:

Chai Dong¹,Fang Yang-Wang²,Peng Wei-Shi²,Yang Peng-Fei²

Affiliation:

1. Department of Flight Vehicle and Power Engineering, School of Aeronautics and Astronautics Engineering, Air Force Engineering University, Xi'an, PR China

2. Department of Aerospace Weapon Engineering, School of Aeronautics and Astronautics Engineering, Air Force Engineering University, Xi'an, PR China

Abstract

Numerical simulations are carried out to investigate lateral jet interaction effects for the hypersonic quasi-waverider vehicle. A reasonable jet nozzles layout is proposed. Based on three-dimensional viscous compressible Reynolds Averaged Navier-Stokes codes, comparisons of the jet interaction flow structures between quasi-waverider vehicle and general axisymmetric vehicle are conducted. Furthermore, the effects of lateral jet control are examined for different angles of attack and free-stream Mach numbers. From detailed flow structure and pressure distribution analysis, the quasi-waverider vehicle gets a better effect of lateral jet without “wrap-around” the body. With the increase in angle of attack or free-stream Mach number, the attitude control moment reduces and the effect of lateral jet decreases.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1177/0954410015586840

Reference9 articles.

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