Design and Study of Swirl Injector of Pulse Detonation Engine
Journal: International Journal of Advanced Engineering Research and Science (Vol.4, No. 4)Publication Date: 2017-04-08
Authors : Navdeep Banga; Kanika;
Page : 79-82
Keywords : detonation engines; detonation; PDE; PDE ignition; swirl injector.;
Abstract
Future Indian Air force and Navy Capabilities indicate the need for a supersonic cruise missile. Therefore, there exists a need for a low cost, light-weight, and efficient means of supersonic propulsion. In this paper my main emphasis on Pulse Detonation Engine, in pulse detonation engine humphey cycle is used ,PDE has thermodynamic efficiency greater than 50% as compared to 35% for present day propulsion technology constant-pressure Brayton cycle currently in use in gas turbines/ramjets/scramjets. Pulse Detonation Engines (PDE’s) represent an upcoming new approach to propulsion and with the simplicity of its construction; PDE’s produce thrust more efficiently than the current engines and produces a higher specific thrust. Since current rocket engines require heavy and expensive pumps; with mechanical simplicity and thermodynamic efficiency PDE’s offer a viable alternative to reduce the cost of launching spacecraft.
Other Latest Articles
- ITIL Implementation in a Moroccan Stat Organization: The case of incident management process
- THE ANALYSIS OF THE DEGREE OF FULFILLMENT OF TARGETS FOR ENERGY AND ENVIRONMENT IN THE EU SUSTAINABLE DEVELOPMENT STRATEGY
- DETERMINATION OF HYDRAULIC TURBINE EFFICIENCY BY MEANS OF THE CURRENT METER METHOD
- SOLUTIONS WITH DIFFERENTIAL PRESSURE IN HEATING WITH RADIATORS
- DETERMINATION OF ATTENUATION INDEX CURVE "Ri(f)" FOR HOMOGENEOUS DOUBLE LOCKING ELEMENTS
Last modified: 2017-04-15 20:31:02