Analysis of Scramjet Flight Trajectories with Oxygen Enrichment [PDF]
, 2007 Scramjets are proposed as a second stage for a multi-stage access-to-space system. At present the upper limit of scramjet operation is expected to be Mach 12-14.
N. Weidner +5 more
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Usage of extruded diamond multi-injectors for improvement of fuel mixing inside the supersonic combustion chamber. [PDF]
Sci Rep, 2023 Seraj H +3 more
europepmc +1 more source
, 2014 The performance of a hypersonic flight vehicle will depend on existing materials and fuels; this work presents the performance of the ideal scramjet engine for three different combustion chamber materials and three different candidate fuels.
Choi, Jongseong
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Constant Velocity Combustion Scramjet Analysis
, 2016 The supersonic combustion ramjet or scramjet, is the most suitable engine cycle for sustained hypersonic flight in the atmosphere. The present work deals with the performance of a scramjet engine by parametrically analyzing the performance of the ideal ...
Tiruveedula, Lakshmi Srikanth
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The SCRAMSPACE I scramjet flight design and construction
, 2012 The design activities of the development of the SCRAMSPACE I scramjet-powered free-flight experiment are described in this paper. The objectives of this flight are first described together with the definition of the primary, secondary and tertiary ...
Boyce, Russel R. +18 more
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Influence of extruded injector nozzle on fuel mixing and mass diffusion of multi fuel jets in the supersonic cross flow: computational study. [PDF]
Sci Rep, 2023 Abdollahi SA +2 more
europepmc +1 more source
Experimental Studies on Scramjet Tested in a Freejet Facility
, 2004 Two different type scramjet models with side-wall compression and top-wall compression inlets have been tested in HPTF (Hypersonic Propulsion Test Facility) under the experimental conditions of Mach number 5.8, total temperature 1700K, total pressure 4 ...
俞刚, 张新宇, 顾洪斌, 陈立红
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Scramjet testing in the T4 impulse facility
, 1998 Scramjet testing in the free piston driven shock tunnel T4 has been undertaken for the past 10 years with a range of experiments spanning diagnostic pressure measurements hi simple combustors to force measurements on complete and integrated scramjet ...
R. Stalker +3 more
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Tunable Diode Laser Absorption Spectroscopy Based Temperature Measurement with a Single Diode Laser Near 1.4 μm. [PDF]
Sensors (Basel), 2022 Liu X, Ma Y.
europepmc +1 more source
Experimental Studies on Model Scramjet in a Mach 6 High Enthalpy Free-Jet Wind Tunnel
, 2005 A side-wall compression scramjet model with different combustor geometries has been tested in a propulsion tunnel that typically provides the testing flow with Mach number of 5.8, total temperature of 1800K, total pressure of 4.5MPa and mass flow rate of
Chen LH(陈立红) +4 more
core +1 more source