COMPUTATIONAL INVESTIGATION OF TRANSVERSE FUEL-INJECTION SCRAMJET COMBUSTOR FOR DIFFERENT INCOMING MACH NUMBERS
Author:
Publisher
Begell House
Subject
General Medicine
Link
https://www.dl.begellhouse.com/download/article/61ee69c153d80773/FMR4905(3)-43291.pdf
Reference74 articles.
1. Ambe Verma, K., Murari Pandey, K., and Kumar Sharma, K., Effect of Wall Cavity with Combined Fuel Injection Technique in Scramjet Combustor with CFD, Mater. Today: Proc, 2021a. DOI: 10.1016/j.matpr.2020.11.787
2. Ambe Verma, K., Murari Pandey, K., Ray, M., and Kumar Sharma, K., Effect of Transverse Fuel Injection System on Combustion Efficiency in Scramjet Combustor, Energy, vol. 218, p. 119511,2021b. DOI: 10.1016/j.energy.2020.119511
3. Ansys, ANSYS Fluent Theory Guide 15.0, Canonsburg, PA: ANSYS Inc., 2013.
4. Baurle, R.A., Mathur, T., Gruber, M.R., and Jackson, K.R., A Numerical and Experimental Investigation of a Scramjet Combustor for Hypersonic Missile Applications, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. Exhibit, 1998. DOI: 10.2514/6.1998
5. Bordoloi, N., Alontseva, D., Pandey, K.M., and Sharma, K.K., The Performance of a Scramjet Combustor with Cavity for Mach Numbers 2.25,2.52 and 2.75 with Hydrogen as a Fuel, Mater. Today:: Proc., vol. 45, pp. 6615-6622,2020.
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