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industrie mécanique - iate.europa.eu
industrie mécanique - iate.europa.eu
Method for calculation of ram-jet performance /A method utilizing precalculated solutions graphically presented for calculating subsonic and supersonic ram-jet thrust coefficients and other important quantities is presented with the associated equations and graphs....
général - core.ac.uk - PDF: www.hathitrust.org
industrie mécanique - iate.europa.eu
Flight investigation of a ram jet burning magnesium slurry fuel and having a conical shock inlet designed for a mach number of 4.1 /A flight investigation was made of a rocket-launched ram-jet engine incorporating an inlet designed for a Mach number of 4.1...
général - core.ac.uk - PDF: www.hathitrust.org
[photograph 2012.201.b1321.0133]... Caption: "University of Oklahoma aeronautical engineering students Wanda Little and James White, both of Oklahoma City, invite you to inspect this ram-jet engine on an experimental helicopter to be at the Engineer's Open House, Friday and Saturday, by the OU School of Aeronautical Engineering.
Investigation of three low-temperflture-ratio combustor configurations in a 48-inch-diameter ram-jet engineA preliminary evaluation was made of three types of combustor con-figuration in a 48-inch-diameter ram-jet engine in order to select the one with the greatest promise of efficient and stable combustion at low fuel-air ratios and low combustor-inlet pressures....
Design of combustor for long-range ram-jet engine and performance of rectangular analogThis report describes the design of a piloted combustor intended for a ram-jet engine of long f l igh t range....
Investigation of an on-off inut shock-position control on a 16-inch ram-jet engine.A shock-positioning control w i s imestigateii mi 8 i6-inch ram- jet engine at Mach numbers from 1.5...
industrie mécanique - iate.europa.eu
Correction of ramjet experimental data... Other names have also been proposed such as athodyd, which is a contraction of aero-thermodynamic duct.The...
général - core.ac.uk - PDF: thesis.library.caltech.edu
industrie mécanique - iate.europa.eu
Fifty years of hypersonics: where we've been, where we're going... Such problems include: the ineffectiveness of the body flap for the Space Shuttle Orbiter, the viscous/inviscid interactions produced by the umbilical fairings that damaged the conical section tile protection system of the Gemini Capsule, and the shock/shock interaction that damaged the X-15A-2 when it carried the hypersonic ramjet experiment....
général - core.ac.uk - PDF: digitalcommons.calpoly.edu
Atomic recombination in nozzles: methods of analysis for flows with complicated chemistry- by-...feasibility of performing accurate calculations on the non-equilibzWm flow of a complicated gas mixture through nozzles, with partioular reference to the propulsive nozzle of the hypersonic ramjet....
H2 fueled flightweight ramjet construction and test... An 18 inch hypersonic ramjet evaluation scale model was designed based on the hot test results using a fully V/G inlet and exit nozzle....
industrie mécanique - iate.europa.eu
Theory and design of flight-vehicle engines...experimental determination of the parameters of scramjet engines, the effect of the nonuniformity of supersonic flow with shocks on friction and heat transfer in the channel of a hypersonic ramjet engine, and the selection of the basic parameters of cooled GTE turbines....
général - core.ac.uk - PDF: hdl.handle.net
A survey of hypersonic-ramjet conceptsA brief discussion is presented of the major problem areas involved in the development of a hypersonic ramjet engine....
industrie mécanique - iate.europa.eu
A model for the performance of air-breathing pulse detonation engines... Performance calculations are carried out for pulse detonation engines operating with stoichiometric hydrogen-air and JP10-air and compared to the performance of the ideal ramjet....
industrie mécanique / technologie et réglementation technique - core.ac.uk - PDF: www2.galcit.caltech.edu
industrie mécanique - iate.europa.eu

Publications scientifiques

Installed performance evaluation of an air turbo-rocket expander engine AbstractThe propulsion plant of a prospective supersonic cruise aircraft consists of an air turbo-rocket expander and a dual-mode ramjet....
détérioration de l'environnement / transports aérien et spatial / organisations européennes - core.ac.uk -
Aprrformanceanalysis ofmethods forhandltng excess inlet flow at supersonic spezds... The following techniques were examined and evaluated in terms of their respective thrust penalties for an assumed turbojet engine: normal- and olique-shock spilhe, by-passing through an auxiliary exit, bypassing to an ejector exhaust nozzle, and, finally, bypassing the excess flow through an auxilisry ramjet engine....
transports aérien et spatial - core.ac.uk - PDF: digital.library.unt.edu
Air breathing rocket engines and sustainable launch systems... Air breathing rockets, combine the performance characteristics of both rocket and ramjet engines....
détérioration de l'environnement / industrie mécanique / organisation des transports - core.ac.uk - PDF: www.scientific.net
Investigative ramjet tests of the erjv ejector ramjetAn investigation has been carried out to evaluate the design of the ERJV ejector ramjet combustor....
général - core.ac.uk - PDF: nal-ir.nal.res.in

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sciences naturelles et appliquées - iate.europa.eu
politique des transports / sciences naturelles et appliquées - iate.europa.eu
politique des transports / sciences naturelles et appliquées - iate.europa.eu
politique des transports / sciences naturelles et appliquées - iate.europa.eu


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