Numerical Study of Effect of Fuel Injection Angle on the Performance of a 2D Supersonic Cavity Combustor-Reference-Cited by-同舟云学术

Numerical Study of Effect of Fuel Injection Angle on the Performance of a 2D Supersonic Cavity Combustor

Published:2012-04 Issue:2 Volume:25 Page:161-167
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Mishra D. P.¹,Sridhar K. V.²

Affiliation:

1. Dept. of Aerospace Engineering, Indian Institute of Technology, Kanpur-208 016, India (corresponding author).

2. Dept. of Aerospace Engineering, Indian Institute of Technology, Kanpur-208 016, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000093

Reference16 articles.

1. Abdel-Salam T. M. and Carson R. A. (2004). “Three-dimensional numerical study of a dual-mode scramjet combustor.” 37th AIAA Thermophysics Conf. AIAA-2002-805 American Institute of Aeronautics & Astronautics Reston VA.

2. Baurle R. A. Eklund D. R. and Gruber M. R. (2001). “Numerical study of scramjet combustor fueled by aerodynamic ramp injector in dual mode combustion.” AIAA Conf. AIAA Reston VA 0379.

3. Fluent 6.3 [Computer software]. (2006). Fluent Inc. Lebanon NH.

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