Tīmeklis2012. gada 23. maijs · American Institute of Aeronautics and Astronautics 12700 Sunrise Valley Drive, Suite 200 Reston, VA 20241-5807 703.264.7500 Tīmeklis1990. gada 18. jūn. · Planar measurements of injectant mole fraction and temperature have been conducted in a nonreacting supersonic combustor configured with underexpanded injection in the base of a swept ramp. The temperature measurements were conducted with a Mach 2 test section inlet in streamwise planes perpendicular …
Scramjet Operability Range Studies of an Integrated Aerodynamic …
Tīmeklis2014. gada 10. marts · The combustion field downstream of a 10 deg compression ramp injector has been studied experimentally using wall static pressure measurement, … TīmeklisFor V. BOUNDARY CONDITIONS the case with central injector, the first pressure peaks are Three types of boundaries are applied: inflow, outflow and produced by the shock formed at the inlet-compression ramp, fixed walls and the entire flow field is considered to be and then the shock goes under the cowl and impacts supersonic. how to turn on hibernation windows 10
AC Motor Braking Methods Ramp, Coast, DC …
Tīmeklis2014. gada 1. jūn. · A computational study of a scramjet combustor with swept ramp fuel injectors was conducted with the SPARK Navier-Stokes computer code, Turbulence … Tīmeklis2015. gada 5. sept. · In the current study, the cantilevered ramp injector was used to promote mixing of the fuel and the supersonic flow, and the injector’s configuration … TīmeklisA multi-height ramp injection system (12), for use in a supersonic propulsion system (16), comprises a plurality of multi-height ramp injectors (30, 32) for variably … ord to stl flight time