Results 81 to 90 of about 139,373 (174)
Thermal compression effects within a fundamental, hydrogen-fuelled scramjet
, 2021 The impact of thermal compression on combustion has been studied experimentally in a hydrogen-fuelled, non-uniform scramjet flowpath. The experimental model consisted of a three-dimensional inlet, a constant area rectangular combustor, and a single-ramp ...
Vanyai, Tristan +4 more
core +1 more source
Numerical simulation of scramjet inlet flow fields [PDF]
, 1986 A computer program was developed to analyze supersonic combustion ramjet (scramjet) inlet flow fields. The program solves the three-dimensional Euler or Reynolds averaged Navier-Stokes equations in full conservation form by either the fully explicit or ...
Kumar, Ajay
core
Tradeoffs in jet inlet design: a historical perspective
, 2007 The design of the inlet(s) is one of the most demanding tasks of the development process of any gas turbine-powered aircraft. This is mainly due to the multi-objective and multidisciplinary nature of the exercise.
András Sóbester, Sóbester, András
core +1 more source
AerospaceConventional forward bleed slots reduce the hypersonic inlet starting Mach number but suffer from excessive flow leakage after restart. This paper proposes a novel reverse bleed slot design method for curved axisymmetric inlets of a solid-fuel scramjet ...
Yongzhou Li +5 more
doaj +1 more source
International Journal of Aerospace Engineering, 2019 In order to overcome the drag at hypersonic speed, hypersonic flight vehicles require a high level of integration between the airframe and the propulsion system.
Sergio Nicolas Pachón Laitón +4 more
doaj +1 more source
A Computational and Experimental Investigation of a Three-Dimensional Hypersonic Scramjet Inlet Flow Field [PDF]
, 1991 A combined computational and experimental parametric study of the internal aerodynamics of a generic three dimensional sidewall compression scramjet inlet configuration was performed.
Holland, Scott Douglas
core
Aerodynamic Configuration Design for Wide-Speed-Range Vehicles and Morphing Effectiveness Analysis
气体物理This study focused on the critical technologies for wide-speed-range high-speed vehicle design, particularly the integration of aerodynamic configuration and adaptive morphing flight strategies.
Lipeng QU +6 more
doaj +1 more source
Physical insight into scramjet inlet behavior via multi-objective design optimization
, 2012 Scramjet propulsion is a promising technology for reliable and economical access to space and high-speed atmospheric transport. The inlet plays a key role in determining the performance of scramjets, in particular for the axisymmetric class of scramjet ...
Ogawa, Hideaki, Boyce, Russell R.
core +2 more sources
Case Studies in Thermal EngineeringA Thermoelectric Conversion System (TECS) with SCO2 as the circulating mass can effectively mitigate the fuel heat sink and electrical energy shortage problems of hypersonic vehicles.
Xiaojuan Niu +5 more
doaj +1 more source
Numerical Investigation of Fuel Cooling in Sudden Expansion Structures of Scramjet Engines
AerospaceLocal overheating in cavities seriously threatens the safe operation of scramjet engines. To investigate the formation mechanism and control methods of local overheating, this paper conducts numerical simulations on the cooling process of cavity sudden ...
Qingjun Wang +3 more
doaj +1 more source