INVESTIGATION OF SCRAMJET INJECTION STRATEGIES FOR HIGH MACH NUMBER FLOWS

Authors
RIGGINS DW MCCLINTON CR ROGERS RC BITTNER RD
Citation
Dw. Riggins et al., INVESTIGATION OF SCRAMJET INJECTION STRATEGIES FOR HIGH MACH NUMBER FLOWS, Journal of propulsion and power, 11(3), 1995, pp. 409-418
Citations number
17
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
Journal of propulsion and power → ACNP
ISSN journal
07484658
Volume
11
Issue
3
Year of publication
1995
Pages
409 - 418
Database
ISI
SICI code
0748-4658(1995)11:3<409:IOSISF>2.0.ZU;2-S
Abstract
A method for estimating the axial distribution of thrust performance p otential in a supersonic combustor is described, A complementary techn ique for illustrating the spatial evolution and distribution of thrust potential and loss mechanisms in reacting flows is developed. A wall jet case and swept ramp injector case for Mach 17 and Mach 13.5 flight enthalpy inflow conditions, respectively, are numerically modeled and analyzed using these techniques.