Research on HIFiRE project's hypersonic vehicle integrated design of aerodynamic and scramjet propulsion

Deng Fan; Ye Youda; Jiao Zihan; Liu Hui

doi:10.11729/syltlx20160125

Volume 31 Issue 2

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Journal of Experiments in Fluid Mechanics > 2017 > 31(2): 73-80. > DOI: 10.11729/syltlx20160125

Deng Fan, Ye Youda, Jiao Zihan, Liu Hui. Research on HIFiRE project's hypersonic vehicle integrated design of aerodynamic and scramjet propulsion[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(2): 73-80. DOI: 10.11729/syltlx20160125

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Research on HIFiRE project's hypersonic vehicle integrated design of aerodynamic and scramjet propulsion

Deng Fan^{1, 3, ,},
Ye Youda²,
Jiao Zihan¹,
Liu Hui¹

1.
Science and Technology on Space Physics Laboratory, China Academy of Launch Vehicle Technology, Beijing 100191, China
2.
National Laboratory for Computational Fluid Dynamics, China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China
3.
Department of Mechanical Engineering, University of Sheffield, Sheffield S13 JD, UK

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Received Date: August 24, 2016
Revised Date: September 29, 2016

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Abstract

Abstract

By the HIFiRE project, America and Australia have deeply investigated the aerodynamics, propulsion and controlling system of hypersonic aircrafts. The high-speed ability is evaluated for the integrated design of aircrafts with propulsion system. A series of valuable flight-data and staged achievements are obtained by the flight tests of single-target evaluation and step-by-step improvement, the principal study of waverider shapes and different propulsion systems, and the verification of designing condition by flight tests. The key technique and experimental conclusion are summarized for the overall design by organizing the flight tests of dynamics/propulsion integrated processes. Moreover, the developing trend is analyzed for the aircraft with propulsion system. The results show that the unit Reynolds number of the transition is between 3×10⁶ and 4×10⁶, and a combination of scramjet and waverider with high lift characteristics at small attack angle is the optimized design, which gives some suggestions for the overall design of high-speed aircrafts with scramjet.
- aerodynamic layout,
- propulsion system,
- integrated design,
- hypersonic,
- flight test

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