506
Views
8
CrossRef citations to date
0
Altmetric
Original Articles

Analysis on Mode Transition in a Dual-Mode Scramjet Combustor

, , &
Pages 82-96 | Received 26 Feb 2017, Accepted 02 Sep 2017, Published online: 25 Sep 2017

References

  • Bao, H., Zhou, J., and Pan, Y. 2017. The effect of kerosene injection on ignition probability of local ignition in a scramjet combustor. Acta Astronaut., 132, 54–58.
  • Bouchez, M. 2001. Dual-mode ramjet thermo-mechanical design and associated performance. Paper AIAA-2001-1918. Presented at the 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, April 24–27.
  • Heiser, W.H., and Pratt, D.T. 1994. Hypersonic Airbreathing Propulsion, AIAA, Washington, DC, pp. 391–392.
  • Huang, W., and Yan, L. 2016. Numerical investigation on the ram-scram transition mechanism in a strut-based dual-mode scramjet combustor. Int. J. Hydrogen Energy, 41, 4799–4807.
  • Li, X., Liu, W., Pan, Y., Yang, L., An, B., & Zhu, J. 2017. Characterization of kerosene distribution around the ignition cavity in a scramjet combustor. Acta Astronaut., 134, 11–16.
  • Lin, K.C., Tam, C.J., Eklund, D.R., Jackson, K.R., and Jackson, T.A. 2006. Effect of temperature and heat transfer on shock train structures inside constant-area isolators. Paper AIAA-2006-817. Presented at the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9–12.
  • Lin, K.C., Tam, C.J., Jackson, K.R., Eklund, D.R., and Jackson, T.A. 2006. Characterization of shock train structures in-side constant-area isolator of model scramjet combustor. Paper AIAA-2006-816. Presented at the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9–12.
  • Mahto, N.K., Choubey, G., Suneetha, L., & Pandey, K. M. 2016. Effect of variation of length-to-depth ratio and Mach number on the performance of a typical double cavity scramjet combustor. Acta Astronaut., 128, 540–550.
  • Smith, T.B. 2001. Development and ground testing of direct measuring skin friction gages for high enthalpy supersonic flight tests. Virginia Polytechnic Institute and State University. PhD dissertation. Blacksburg, VA.
  • Sullins, G.A., Carpenter, D.A., and M.W. Thompson, M.W. 1991. A demonstration of mode transition in a scramjet combustor. Paper AIAA-91-2395. Presented at the 27th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Sacramento, CA, June 24–27.
  • Tang, M., and Chase, R.L. 2008. The quest for hypersonic flight with air-breathing propulsion. Paper AIAA-2008-2546. Presented at the 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, April–May.
  • Tomioka, S., Kobayashi, K., Nojima, K., and Ishizaki, S. 2015. On mode-transition within diverging dual-mode combustors. Paper AIAA-2015-4142. Presented at the 51st AIAA/SAE/ASEE Joint Propulsion Conference, Orlando, FL, July 27–29.
  • Zhang, C., Chang, J., Zhang, Y., Wang, Y., & Bao, W. 2017. Flow field characteristics analysis and combustion modes classification for a strut/cavity dual-mode combustor. Acta Astronautica. 137, 44–51.

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.