INTERACTIONS BETWEEN SHOCKWAVES AND COMBUSTION PROCESS OF RAMJET AND SCRAMJET ENGINES - A REVIEW
| Author(s) | : | Lakshay Bansal, Manish Kumar Bharti |
| Institution | : | Department of Aerospace Engineering, Amity University Haryana, Gurugram, India |
| Published In | : | Vol. 5, Issue 4 — April 2018 |
| Page No. | : | 1193-1198 |
| Domain | : | Engineering |
| Type | : | Research Paper |
| ISSN (Online) | : | 2348-4470 |
| ISSN (Print) | : | 2348-6406 |
Shocks are utilizedat many stages in the operation of ramjet and scramjet engines.Shock isgenerated due tosudden change in flow properties and is used in diffusor and in nozzle expansion of high speed jet engines. Shocks maybe stable or unstable depending on the design and cross-section of the region in which it is generated and advancing.The transition of air flow from supersonic speeds to subsonic speeds in ramjet enginestakes place through generation ofshock. Gases in nozzle are also accelerated through shock generation. Vortices created due to shockwaves are used inscramjet engines for faster diffusion of air and fuel leading to efficient combustion process. The present study reviewsand compares the various aspect of shock generation and shock flow interaction in both ramjet and scramjet engines.
Lakshay Bansal, Manish Kumar Bharti, “INTERACTIONS BETWEEN SHOCKWAVES AND COMBUSTION PROCESS OF RAMJET AND SCRAMJET ENGINES - A REVIEW”, International Journal of Advance Engineering and Research Development (IJAERD), Vol. 5, Issue 4, pp. 1193-1198, April 2018.
