Works matching DE "ROCKET engine combustion"

Results: 19

Effect of distributed injection of air into the afterburning chamber of a ram-rocket engine on the efficiency of combustion of boron particles.

Published in:

Combustion, Explosion, & Shock Waves, 2017, v. 53, n. 6, p. 652, doi. 10.1134/S0010508217060053

By:

Rashkovskii, S.;
Milekhin, Yu.;
Fedorychev, A.

Publication type:

Article

Diagnostics of acoustic properties of the combustion zone by means of periodic changes in the nozzle throat area.

Published in:

Combustion, Explosion, & Shock Waves, 2008, v. 44, n. 6, p. 627, doi. 10.1007/s10573-008-0096-8

By:

Lisochkin, Ya.

Publication type:

Article

Thermal Decomposition and Combustion of Ammonium Dinitramide (Review).

Published in:

Combustion, Explosion, & Shock Waves, 2005, v. 41, n. 6, p. 657, doi. 10.1007/s10573-005-0079-y

By:

Yang, R.;
Thakre, P.;
Yang, V.

Publication type:

Article

Radiative Heating in Combustion Chamber of Liquid Propellant Rocket Engines.

Published in:

Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 332, doi. 10.2322/tjsass.59.332

By:

Takeshi KANDA;
Masaki SATO

Publication type:

Article

Thermodynamic substantiation of the existence of a phase transition point with a change in the structure of the solid-fuel mixture glycidyl azide Polymer/RDX.

Published in:

Journal of Engineering Physics & Thermophysics, 2012, v. 85, n. 5, p. 1058, doi. 10.1007/s10891-012-0747-1

By:

Futko, S.

Publication type:

Article

Design optimization of a methane-fuel rocket combustor with a genetic algorithm.

Published in:

Journal of Mechanical Science & Technology, 2015, v. 29, n. 4, p. 1457, doi. 10.1007/s12206-015-0318-4

By:

Son, Min;
Koo, Jaye;
Kim, Byungkyu;
Jang, Seok;
Lee, Jaewook

Publication type:

Article

Flight Overloading Effect on the Working-Process Instability in the Combustion Chamber of a Solid-Fuel Rocket Engine.

Published in:

Doklady Physics, 2004, v. 49, n. 9, p. 527, doi. 10.1134/1.1810579

By:

Davydov, Yu. M.;
Davydova, I.M.;
Egorov, M. Yu.

Publication type:

Article

Numerical Evaluation of the Use of Aluminum Particles for Enhancing Solid Rocket Motor Combustion Stability.

Published in:

Energies (19961073), 2015, v. 8, n. 2, p. 1195, doi. 10.3390/en8021195

By:

Greatrix, David

Publication type:

Article

Mechanical Properties of Gel Propellants with Nanoparticles.

Published in:

Journal of Energetic Materials, 2004, v. 22, n. 2, p. 69, doi. 10.1080/07370650490492824

By:

TEIPEL, U.;
FOERTER-BARTH, U.

Publication type:

Article

Contact diagnostics of combustion products of rocket engines, their units, and systems.

Published in:

Solar System Research, 2013, v. 47, n. 7, p. 582, doi. 10.1134/S0038094611070094

By:

Ivanov, N. N.;
Ivanov, A. N.

Publication type:

Article

Analysis of Coolant Mass Flow Requirements for Transpiration Cooled Ceramic Thrust Chambers.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 31

By:

Herbertz, Armin;
Selzer, Markus

Publication type:

Article

Combustion Phenomena within a RBCC Engine under Scramjet-mode Operation.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 71

By:

Tomoyuki KOMURO;
Sadatake TOMIOKA;
Masahiro TAKAHASHI;
Shuichi UEDA;
Katsuhiro ITOH;
Shohei TAKAGI

Publication type:

Article

Numerical Study of Real Gas Effects on Shock Tube Problems at Supercritical Conditions.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 39

By:

Daiki MUTO;
Nobuyuki TSUBOI;
Hiroshi TERASHIMA

Publication type:

Article

A Study on Combustion Efficiency Improvement of Low Melting Temperature Thermoplastics as a Hybrid Rocket Fuel.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 9

By:

Yutaka WADA;
You KAWABATA;
Kotaro SHINNAKAZAKI;
Ryuichi KATO;
Nobuji KATO;
Keiichi HORI

Publication type:

Article

Development and Ground Combustion Test of a Subscale Reusable Winged Rocket.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1

By:

Kyoshiro ITAKURA;
Gaku SASAKI;
Shintaro MIYAMOTO;
Hiroshi YAMASAKI;
Takaaki MATSUMOTO;
Koichi YONEMOTO

Publication type:

Article

373. INFLUENCE OF OVERLOAD ON LOW-FREQUENCY INSTABILITY OF WORKING PROCESS IN THE COMBUSTION CHAMBER OF THE SOLID PROPELLANT ROCKET ENGINE.

Published in:

Journal of Vibroengineering, 2008, v. 10, n. 3, p. 272

By:

Davydov, Yu. M.;
Davydova, I. M.;
Egorov, M. Yu.

Publication type:

Article

International symposium on thermoacoustic instabilities in gas turbines and rocket engines: Industry meets academia.

Published in:

2017

By:

Schuermans, Bruno

Publication type:

Proceeding

The use of OH* and CH* as heat release markers in combustion dynamics.

Published in:

International Journal of Spray & Combustion Dynamics, 2017, v. 9, n. 4, p. 409, doi. 10.1177/1756827717718483

By:

Sardeshmukh, Swanand;
Bedard, Michael;
Anderson, William

Publication type:

Article

Determination of a Two Variable Approximation Function with Application to the Fuel Combustion Charts.

Published in:

INCAS Bulletin, 2017, v. 9, n. 3, p. 3, doi. 10.13111/2066-8201.2017.9.3.1

By:

ANDREI, Irina-Carmen

Publication type:

Article