Results 91 to 100 of about 2,233 (228)
Numerical Modelling of Liquid Ramjet Combustors [PDF]
, 2008 The liquid fuel ramjet system employing a subsonic side-dump combustor is simulated inthe present study, and the predictions are compared with the available experimental data.
Babu, V. +3 more
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Experimental Research of Supersonic Flow Around Simulating Rocket-Ramjet
MATEC Web of Conferences, 2015 The results of experimental researches of the structure and of the basic parameters of the air when flow around flat and axisymmetric models of rocket-ramjet engine are presented.
Maslov Eugene A. +2 more
doaj +1 more source
Numerical investigation of second-law characteristics of ramjet throttling [PDF]
, 2012 A numerical study of a generic axisymmetric ramjet operating at conditions corresponding to flight Mach 3.0 and a standard altitude of 10 km is presented.
Sheldon, Jonathan Albert
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The performance of a boron-loaded gel-fuel ramjet [PDF]
, 2011 The present work focuses on the possibility of combining the advantages of ramjet propulsion with the high energetic potential of boron. However, the use of boron poses two major challenges.
R. Arieli, B. Natan, A. Haddad
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Study of heat transfer processes in the flowing part of hypersonic air-ramjet engine
MATEC Web of Conferences, 2018 The technique and results of the experimental-theoretical study of gas dynamics, heat transfer and the structure of gas flow in the flowing channel of a model hypersonic air-ramjet engine are presented for Mach numbers M = (5; 6).
Maslov Eugene +4 more
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The equation of motion of an interstellar Bussard ramjet [PDF]
, 2005 An interstellar Bussard ramjet is a spaceship using the protons of the interstellar medium in a fusion engine to produce thrust. The velocity of an ideal ramjet (100% efficient hydrogen fusion engine) could, in theory, approach the speed of light in a ...
Semay, C. +2 more
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COMPUTATIONAL ANALYSIS OF THE MIXING ZONE IN THE COMBUSTION CHAMBER OF RAMJET
Iraqi Journal of Chemical and Petroleum Engineering, 2008 A theoretical analysis of mixing in the secondary combustion chamber of ramjet is presented. Theoretical investigations were initiated to insight into the flow field of the mixing zone of the ramjet combustor and a computer program to calculate ...
Adil A. Al-Hemiri, Sa’ad A. Fa’ek
doaj
NUMERICAL SIMULATIONS OF INVISCID AIRFLOWS IN RAMJET INLETS [PDF]
, 2009 The performances of three different ramjet inlets and an entire ramjet are numerically studied in this paper. The fluid is assumed to be inviscid. Inlet 1 is a SCRAMJET inlet and is chosen from the literature.
M. J. Kermani, M. Akbarzadeh
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Hyplane: a single-stage suborbital aerospaceplane. [PDF]
CEAS Space J, 2023 Russo G, Voto C.
europepmc +1 more source
Numerical and experimental investigation of direct connected ramjet test facility [PDF]
, 2014 The main objective of this study is to make a numerical model of direct connected ramjet test facility which is used for ground tests of supersonic air breathing propulsion systems.
BAŞAR ESİRGEN
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