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Estimation of parameters of a pulse detonation engine (РDЕ)
Anakin A.T., Tsybizov Y.I.
Design procedure of fundamental parameters of the direct-flow detonation pulsing engine
Porshnev V.A.
Evaluation of the possibility of using combustion promoters in hydrocarbon fuels for perspective jet engines
Petrukhin N.V., Sergeev S.M., Prokopenko O.A., Grek M.O.
Manipulate pulsed detonation engine
1 1., 1 1.
Multicriterial choice of the best variant of the pulse detonation engine design for aircraft angular stabilization and orientation systems
Safronov V.V., Porshnev V.A., Zhebrakov A.S.
Gas dynamic calculation of detonation in constant-cross-section ducts
Grigoriev A.V., Rudakov O.A., Solovieva A.V.
Technique of conclusion the direct-flow detonation pulsing engine design to the leader position
Safronov V.V., Porshnev V.A., Zhebrakov A.S.
Some results of experimental refining of a constant volume valve combustion chamber
Bogdanov V.I., Kuznetsov S.P.
Theory and calculation of parameters of the detonation engine thermodynamical cycle
Grigoriev A.V., Mitrofanov V.A., Rudakov O.A., Solovieva A.V.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
1 - 10 of 10 Items

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