Results 161 to 170 of about 10,850 (227)

Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber. [PDF]

Sci Rep
Alizadeh A, Jasim DJ, Sohrabi N, Ahmed M, Ameer SA, Ibrahim SM, Dabis HK, Hussein AA, Sultan AJ.   +8 more
europepmc   +1 more source

Mesoscopic Kinetic Approach of Nonequilibrium Effects for Shock Waves. [PDF]

Entropy (Basel)
Qiu R, Yang X, Bao Y, You Y, Jin H.
europepmc   +1 more source

Improvement of Water-Cooling Performance for Combustion Chamber Through Optimization of Flow Channel Structure. [PDF]

Materials (Basel)
Wu D, Quan G, Meng F, Li S, Yu Y.
europepmc   +1 more source

Overview of Recent Advances in Rare-Earth High-Entropy Oxides as Multifunctional Materials for Next-Gen Technology Applications. [PDF]

Molecules
Šarić S, Kojčinović J, Tatar D, Djerdj I.   +3 more
europepmc   +1 more source

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Propulsion System for Hypersonic Space Planes

Journal of Propulsion and Power, 2000
Because of its simple construction and low weight, combined rocket, ramjet, pulse-jet engines, or detonation enginesinsteadofturbojets,weretakenintoconsiderationaspropulsionforhypersonicaircraft.Combinedpropulsion requires an active control system to change the propulsion operation mode and to sustain the high-efe cient pulse combustion. Therefore, the
Michael Zeutzius
exaly   +2 more sources

A propulsion for hypersonic space plane

8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 1998
To date, propulsion concepts for advanced space planes are based upon combined engines that include a turbojet as core engine. Turbojets provide sufficient start thrust but also cause a lot of integration problems. Due to its simple construction, combined rocket, ramjet, pulse jet engines or detonation engines instead of turbojets were taken into ...
Michael Zeutzius, Toshiaki Setoguchi, Kunio Terao, Hideo Miyanishi   +3 more
openaire   +1 more source

Analytical Methodologies for Hypersonic Propulsion

46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2010
In this study, we review several analytical frameworks that may be used in the context of high speed propulsion. To this end, inviscid and boundary layer models are examined in the light of modern mathematical techniques. A modified Rayleigh-Janzen approach is offered as a possible improvement over previous inviscid techniques for handling hypersonic ...
Brian Maicke, Timothy Barber, Joe Majdalani   +2 more
openaire   +1 more source