Experimental Studies on Supersonic Cold Flow Mixing with Ramp Mixers-Reference-Cited by-同舟云学术

Experimental Studies on Supersonic Cold Flow Mixing with Ramp Mixers

Published:2005-10 Issue:4 Volume:18 Page:197-205
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Manoharan S.¹²³⁴⁴,Chandra B. Umesh¹²³⁴⁴,Chakravarthy S. R.¹²³⁴⁴,Ramakrishnan S. Rajesh¹²³⁴⁴,Subramanyam J. D.¹²³⁴⁴

Affiliation:

1. Vaiq emer Tek (P) Ltd., Chemnai 600041 India; formerly, Dept. of Aerospace Engineering, Indian Institute of Technology, Madras, Chennai 600 036, India.

2. DLR Aerospace Centre, Cologne 51147 German; formerly, Dept. of Aerospace Engineering, Indian Institute of Technology, Madras, Chennai 600 036, India.

3. Dept. of Aerospace Engineering, Indian Institute of Technology, Madras, Chennai 600 036, India (corresponding author).

4. Vikram Sarabhai Space Centre, Thiruvananthapuram 695 022, 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%290893-1321%282005%2918%3A4%28197%29

Reference20 articles.

1. Mole-fraction imaging of transverse injection in a ducted supersonicflow

2. A planar Mie scattering technique for visualizing supersonic mixing flows

3. Davis D. O. and Hinhst W. R. (1991). “Progress toward synergistic hyper-mixing nozzles.” AIAA Pap.AAPRAQ0146-3705 91–2261.

4. On the two‐way interaction between homogeneous turbulence and dispersed solid particles. I: Turbulence modification

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effects of pulsed hydrogen injection on mixing and combustion performance in a supersonic flow field;Physics of Fluids;2023-10-01

2. Advances in scramjet fuel injection technology;Scramjet Combustion;2022

3. Supersonic mixing in airbreathing propulsion systems for hypersonic flights;Progress in Aerospace Sciences;2019-08

4. Comparison research of two different improved methods in the 2D hypersonic inlet’s design;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2012-12-05

5. Flowfield Characteristics of a Hypermixer Interacting with Transverse Injection in Supersonic Flow;AIAA Journal;2012-08