[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Zhang et al., 2018 - Google Patents

Investigation of performance and mode transition in a variable divergence ratio dual-mode combustor

Zhang et al., 2018

Document ID
9578448521665432112
Author
Zhang C
Chang J
Feng S
Bao W
Yu D
Publication year
Publication venue
Aerospace Science and Technology

External Links

Snippet

To operate in a wide range of incoming flow Mach number, a variable divergence ratio dual- mode combustor is designed. Experimental and numerical investigation of the dual-mode combustor has been conducted in this paper. By regulating the divergence ratio in …
Continue reading at www.sciencedirect.com (other versions)

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles

Similar Documents

Publication Publication Date Title
Zhang et al. Investigation of performance and mode transition in a variable divergence ratio dual-mode combustor
Gnani et al. Pseudo-shock waves and their interactions in high-speed intakes
Feng et al. Experimental and numerical investigation on hysteresis characteristics and formation mechanism for a variable geometry dual-mode combustor
Zhang et al. Flow field characteristics analysis and combustion modes classification for a strut/cavity dual-mode combustor
Mitani et al. Flame structures and combustion efficiency computed for a Mach 6 scramjet engine
Kouchi et al. Mechanism and control of combustion-mode transition in a scramjet engine
Zhang et al. Effect of Mach number and equivalence ratio on the pressure rising variation during combustion mode transition in a dual-mode combustor
Feng et al. Numerical and experimental investigation of improving combustion performance of variable geometry dual-mode combustor
Zhang et al. Effect of continuous Mach number variation of incoming flow on ram–scram transition in a dual-mode combustor
Feng et al. Numerical studies for performance improvement of a variable geometry dual mode combustor by optimizing deflection angle
Nair et al. Combustion efficiency improvement for scramjet combustor with strut based flame stabilizer using passive techniques
Zhang et al. Pressure rising slope variation accompanying with combustion mode transition in a dual-mode combustor
Gnani et al. Numerical investigation on three-dimensional shock train structures in rectangular isolators
Hariharan et al. Investigation on supersonic combustion of hydrogen with variation of combustor inlet conditions
Tian et al. Dynamic characteristics study of regression rate in variable thrust hybrid rocket motor
Shen et al. Characteristics of reaction zone in a dual-mode scramjet combustor during mode transitions
Dong et al. Numerical investigation on flow and mixing characteristics inside a converging-diverging mixing duct of rocket-based combined-cycle engine in ejector mode
McGuire et al. Radical-farm ignition processes in two-dimensional supersonic combustion
Ogawa et al. Effects of leading-edge truncation and stunting on drag and efficiency of Busemann intakes for axisymmetric scramjet engines
Xiang et al. The initiation characteristics of oblique detonation waves induced by a curved surface
Gugulothu et al. Numerical analysis of supersonic combustion of hydrogen flow characteristics in scramjet combustor toward the improvement of combustion efficiency
US20150285506A1 (en) Standing detonation wave engine
Wang et al. Aerodynamic performance enhancement of a variable-geometry dual-mode combustor designed by the method of characteristics
Wei et al. Research on shock wave characteristics in the isolator of central strut rocket-based combined cycle engine under Ma5. 5
Zhuravskaya et al. Stabilization of detonation combustion of a high-velocity combustible gas mixture flow in a plane channel