Works matching DE "SCRAMJET engines"

Results: 145

Triangular tabs for supersonic jet mixing enhancement.

Published in:

Aeronautical Journal, 2014, v. 118, n. 1209, p. 1245, doi. 10.1017/S0001924000009969

By:

Kumar, P. Arun;
Rathakrishnan, E.

Publication type:

Article

Numerical simulations of the flow through the inlet and isolator of a Mach 4 dual mode scramjet.

Published in:

Aeronautical Journal, 2012, v. 116, n. 1182, p. 833, doi. 10.1017/S0001924000007302

By:

Janarthanam, S.;
Babu, V.

Publication type:

Article

Heat transfer characteristic modelling and the effect of operating conditions on re-cooled cycle for a scramjet.

Published in:

Aeronautical Journal, 2011, v. 115, n. 1164, p. 83, doi. 10.1017/S0001924000005479

By:

Bao, W.;
Qin, J.;
Zhou, W. X.

Publication type:

Article

Numerical investigation of the role of hyper-mixers in supersonic mixing.

Published in:

Aeronautical Journal, 2010, v. 114, n. 1161, p. 659, doi. 10.1017/S0001924000004140

By:

Desikan, S. L. N.;
Kumaran, K.;
Babu, V.

Publication type:

Article

The Scramjet Engine: Processes and Characteristics.

Published in:

2010

By:

Zanchetta, Marc

Publication type:

Book Review

A CFD assessment of classifications for hypersonic inlet start/unstart phenomena.

Published in:

Aeronautical Journal, 2009, v. 113, n. 1142, p. 263, doi. 10.1017/S0001924000002931

By:

Chang, J.;
Yu, D.;
Bao, W.;
Xie, Z.;
Fan, Y.

Publication type:

Article

An idea of distributed parameter control for scramjet engines.

Published in:

Aeronautical Journal, 2007, v. 111, n. 1126, p. 787, doi. 10.1017/S0001924000001901

By:

Daren, Y.;
Tao, C.;
Wen, B.

Publication type:

Article

Scramjets.

Published in:

Aeronautical Journal, 2007, v. 111, n. 1124, p. 605, doi. 10.1017/S0001924000004796

By:

Smart, M.

Publication type:

Article

3D numerical simulation of the supersonic combustion of H<sub>2</sub>.

Published in:

Aeronautical Journal, 2006, v. 110, n. 1114, p. 773, doi. 10.1017/S0001924000001640

By:

Dinde, Prashant;
Rajasekaran, A.;
Babu, V.

Publication type:

Article

Effects of hydrogen-air non-equilibrium chemistry on the performance of a model scramjet thrust nozzle.

Published in:

Aeronautical Journal, 2004, v. 108, n. 1089, p. 575, doi. 10.1017/S0001924000000403

By:

Stalker, R.J.;
Truong, N.K.;
Morgan, R.G.;
Paull, A.

Publication type:

Article

The Thermal Correction of the Inlet Diffuser of a Hypersonic Scramjet Engine.

Published in:

High Temperature, 2003, v. 41, n. 3, p. 415, doi. 10.1023/A:1024259130915

By:

Bormotova, T. A.;
Volodin, V. V.;
Golub, V. V.;
Laskin, I. N.

Publication type:

Article

Impact of parametric variation on combustion characteristics of hydrogen‐fueled strut based scramjet combustor at supersonic speed.

Published in:

International Journal of Energy Research, 2020, v. 44, n. 14, p. 11807, doi. 10.1002/er.5822

By:

Verma, Kumari Ambe;
Pandey, Krishna Murari;
Sharma, Kaushal Kumar

Publication type:

Article

Impact of parametric variation on combustion characteristics of hydrogen‐fueled strut based scramjet combustor at supersonic speed.

Published in:

International Journal of Energy Research, 2020, v. 44, n. 14, p. 11807, doi. 10.1002/er.5822

By:

Verma, Kumari Ambe;
Pandey, Krishna Murari;
Sharma, Kaushal Kumar

Publication type:

Article

Study on transient process of mode transition in a scramjet combustor with pilot hydrogen.

Published in:

International Journal of Energy Research, 2018, v. 42, n. 7, p. 2481, doi. 10.1002/er.4030

By:

Xue, Rui;
Xu, Minglong;
Bai, Changqing;
Weng, Chao;
Xu, Chaoqi

Publication type:

Article

Two-line Technique Measurement of Water Vapor in Supersonic Reacted Flow.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2024, v. 22, p. aj19, doi. 10.2322/tastj.22.aj19

By:

Ryota ITO;
Sadatake TOMIOKA

Publication type:

Article

Arrangement of Rocket Engine Location in a Combined Cycle Engine.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 2, p. 165, doi. 10.2322/tastj.17.165

By:

Tatsushi ISONO;
Takahiro FUJIKAWA;
Takeshi TSUCHIYA;
Kan KOBAYASHI;
Masatoshi KODERA;
Kouichiro TANI;
Sadatake TOMIOKA

Publication type:

Article

Breakdown of Counter-Rotating Supersonic Streamwise Vortices Generated by Swept Ramp Injector.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2018, v. 16, n. 2, p. 172, doi. 10.2322/tastj.16.172

By:

Shoji SAKAUE;
Shingo SHICHIRI;
Yamato TSUKAZAKI;
Kazuma HASHIMOTO;
Takakage ARAI

Publication type:

Article

Some Aspects on Hydrocarbon-fueled RBCC Engines for a TSTO Launch Vehicle.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 1

By:

Sadatake TOMIOKA;
Kan KOBAYASHI;
Toshihito SAITO;
Kanenori KATO;
Masatoshi KODERA;
Kouichiro TANI

Publication type:

Article

Numerical Study of Injected Jets into Supersonic Main Flow from a Porous Cavity.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 49

By:

Nao KUNIYOSHI;
Minoru YAGA;
Isao TERUYA;
Masaaki ISHIKAWA

Publication type:

Article

Development of a Small-scale Supersonic Flight Experiment Vehicle as a Flying Test Bed for Future Space Transportation Research.

Published in:

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

By:

Kazuhide MIZOBATA;
Ryojiro MINATO;
Ken HIGUCHI;
Masazumi UEBA;
Syohei TAKAGI;
Daisuke NAKATA;
Kazuyuki HIGASHINO;
Nobuhiro TANATSUGU

Publication type:

Article

Induction Phenomena of Laser Ignition.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 79

By:

Nao AKASHI;
Yoshihiro HARA;
Keisuke KONDO;
Hideyuki HORISAWA

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

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

Published in:

Scientific Reports, 2024, v. 14, n. 1, p. 1, doi. 10.1038/s41598-024-57103-0

By:

Alizadeh, As'ad;
Jasim, Dheyaa J.;
Sohrabi, Neaman;
Ahmed, Mohsen;
Ameer, S. Abdul;
Ibrahim, Safaa Mohammed;
Dabis, Hasan Khalid;
Hussein, Ali Adhab;
Sultan, Abbas J.

Publication type:

Article

Application of multi-extruded fuel injectors for mixing enhancement of hydrogen gas at scramjet engine: computational study.

Published in:

Scientific Reports, 2023, v. 13, n. 1, p. 1, doi. 10.1038/s41598-023-46217-6

By:

Abdollahi, Seyyed Amirreza;
Ranjbar, Seyyed Faramarz;
Aminian, Saman;
Fattahi, M.;
Uyen, P. D.

Publication type:

Article

Fuel mixing enhancement of transverse coaxial air and fuel jet by upstream shock wave on in scramjet engines: numerical study.

Published in:

Scientific Reports, 2023, v. 13, n. 1, p. 1, doi. 10.1038/s41598-023-45810-z

By:

Abdollahi, Seyyed Amirreza;
Jafari, Moharram;
Aminian, Saman;
Fattahi, M.;
Uyen, P. D.

Publication type:

Article

A LES Study on Passive Mixing in Supersonic Shear Layer Flows Considering Effects of Baffle Configuration.

Published in:

Advances in Mechanical Engineering (Sage Publications Inc.), 2014, p. 1, doi. 10.1155/2014/836146

By:

Ren Zhao-Xin;
Wang Bing

Publication type:

Article

Richtmyer-Meshkov Instability Induced Mixing Enhancement in the Scramjet Combustor with a Central Strut.

Published in:

Advances in Mechanical Engineering (Sage Publications Inc.), 2014, p. 1, doi. 10.1155/2014/614189

By:

Qingchun Yang;
Juntao Chang;
Wen Bao

Publication type:

Article

Numerical Investigation on Supercritical Heat Transfer of RP3 Kerosene Flowing inside a Cooling Channel of Scramjet.

Published in:

Advances in Mechanical Engineering (Sage Publications Inc.), 2014, p. 1, doi. 10.1155/2014/213438

By:

Ning Wang;
Yu Pan;
Heng Bao;
Jin Zhou

Publication type:

Article

Mixing Characteristics of Transverse Jet Injection into Supersonic Flow after Rearward-Facing Step.

Published in:

2013

By:

Jinshui Wu;
Hongbo Wang;
Mingbo Sun;
Shunpin Zhang;
Zhenguo Wang

Publication type:

Essay

The fuel mixing of multi-annular extruded fuel jets in cavity flame holder at supersonic combustion chamber: Computational study.

Published in:

International Journal of Modern Physics C: Computational Physics & Physical Computation, 2025, v. 36, n. 3, p. 1, doi. 10.1142/S012918312450195X

By:

Kamyarpour, Naser;
Hosseinnejad, Farhad;
Seyyedi, Seyyed Masoud;
Hashemi-Tilehnoee, M.

Publication type:

Article

SITREP Terrorism Trends & Forecasts 2014.

Published in:

Journal of Counterterrorism & Homeland Security International, 2014, v. 20, n. 3, p. 6

By:

Fustero, Steven J.

Publication type:

Article

Functional mathematical model of a hydrogen-driven combustion chamber for a scramjet.

Published in:

Journal of Applied Mechanics & Technical Physics, 2015, v. 56, n. 5, p. 799, doi. 10.1134/S0021894415050065

By:

Latypov, A.

Publication type:

Article

Shock-unsteadiness model applied to oblique shock wave/turbulent boundary-layer interaction.

Published in:

International Journal of Computational Fluid Dynamics, 2008, v. 22, n. 8, p. 569, doi. 10.1080/10618560802290284

By:

Pasha, Amajad Ali;
Sinha, Krishnendu

Publication type:

Article

Validation of three-dimensional simulation of Flow through Hypersonic air-breathing engine.

Published in:

Defence Science Journal, 2015, v. 65, n. 4, p. 272, doi. 10.14429/dsj.65.6979

By:

Murugan, Thangadurai;
De, Sudipta;
Thiagarajan, V.

Publication type:

Article

Numerical Investigation of Hydrogen-fuelled Scramjet Combustor with Cavity Flame Holder.

Published in:

Defence Science Journal, 2014, v. 64, n. 5, p. 417, doi. 10.14429/dsj.64.5191

By:

Dharavath, Malsur;
Manna, P.;
Chakraborty, Debasis

Publication type:

Article

Evaluation of Kerosene Fuelled Scramjet Combustor using a Combination of Cooled and Uncooled Struts.

Published in:

Defence Science Journal, 2014, v. 64, n. 1, p. 5, doi. 10.14429/dsj.64.2733

By:

Chandrasekhar, C.;
Ramanujachari, V.;
Kumar Reddy, T. Kishen

Publication type:

Article

Computational Fluid Dynamics in Hypersonic Aerothermodynamics.

Published in:

Defence Science Journal, 2010, v. 60, n. 6, p. 663, doi. 10.14429/dsj.60.604

By:

Sinha, Krishnendu

Publication type:

Article

Analysis of inner flow and outflow characteristics of different scramjet elliptical holes.

Published in:

Energy Sources Part A: Recovery, Utilization & Environmental Effects, 2024, v. 46, n. 1, p. 54, doi. 10.1080/15567036.2023.2278719

By:

Kang Zhang;
Bifeng Yin;
Shenghao Yu;
Hekun Jia;
Chen Chen

Publication type:

Article

Performance analysis of a planar shaped strut injector based supersonic combustion chamber.

Published in:

International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 1, p. 205, doi. 10.1515/tjj-2024-0024

By:

Roga, Sukanta

Publication type:

Article

Computational analysis of the scramjet mode of the RBCC inlet using micro vortex generators.

Published in:

International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 1, p. 1, doi. 10.1515/tjj-2024-0015

By:

Raj, Ritul;
Joshi, Ganapati N.;
Chandel, Sunil;
Mishra, Ranjan Kumar

Publication type:

Article

Effect of perforated wall in controlling the separation due to SWBLI at Mach no. 5 to 9.

Published in:

International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 1, p. 59, doi. 10.1515/tjj-2024-0014

By:

Babu R, Dinesh;
Joshi, Ganapati N.;
Chandel, Sunil;
Mishra, Ranjan Kumar

Publication type:

Article

Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity.

Published in:

International Journal of Turbo & Jet-Engines, 2024, v. 41, n. 2, p. 177, doi. 10.1515/tjj-2023-0029

By:

Sanaka, Srinivas Prasad;
Kandula, Ramanaiah;
Chalamalasetty, Khyathi Sree;
Kappala, Durga Rao

Publication type:

Article

Numerical Investigation on the Cold Flow Field of a Typical Cavity-based Scramjet Combustor with Double Ramp Entry.

Published in:

International Journal of Turbo & Jet-Engines, 2022, v. 39, n. 3, p. 439, doi. 10.1515/tjj-2020-0011

By:

Periyasamy, S.;
Ragul, S.;
Sundararaj, K.;
Premkumar, P. S.

Publication type:

Article

Perforated Wall in Controlling the Separation Bubble Due to Shock Wave –Boundary Layer Interaction.

Published in:

International Journal of Turbo & Jet-Engines, 2022, v. 39, n. 2, p. 223, doi. 10.1515/tjj-2018-0048

By:

Raja sekar, K.;
Jegadheeswaran, S.;
Kannan, R.;
Manigandan, P.

Publication type:

Article

Frontmatter.

Published in:: International Journal of Turbo & Jet-Engines, 2019, v. 36, n. 2, p. i, doi. 10.1515/tjj-2019-frontmatter2
Publication type:: Article

Jet-Engines Revised Dictionary for the 6th-Generation-R&D in a New Era: How jet-engines-industries' strategies, designs, R&D and funding are now globally amended.

Published in:

International Journal of Turbo & Jet-Engines, 2019, v. 36, n. 2, p. 127, doi. 10.1515/tjj-2019-9016

By:

Gal-Or, Benjamin

Publication type:

Article

Quasi-One-Dimensional Modeling and Analysis of RBCC Dual-Mode Scramjet Engine.

Published in:

International Journal of Turbo & Jet-Engines, 2019, v. 36, n. 2, p. 195, doi. 10.1515/tjj-2017-0055

By:

Cheng, Feng;
Tang, Shuo;
Zhang, Dong;
Li, Yi

Publication type:

Article

Aerodynamic Optimization of Turbine Based Combined Cycle Nozzle.

Published in:

International Journal of Turbo & Jet-Engines, 2018, v. 35, n. 4, p. 385, doi. 10.1515/tjj-2016-0052

By:

Li, Shangze;
Zhang, Yufei;
Chen, Haixin;
Deng, Kaiwen

Publication type:

Article

Experimental Investigation of Shape Transition Effects on Isolator Performance.

Published in:

International Journal of Turbo & Jet-Engines, 2018, v. 35, n. 4, p. 331, doi. 10.1515/tjj-2015-0022

By:

Chandra Bose, G.;
Thanigaiarasu, S.;
Elangovan, S.;
Rathakrishnan, E.

Publication type:

Article

Experimental Investigation of Reacting Flow Characteristics in a Dual-Mode Scramjet Combustor.

Published in:

International Journal of Turbo & Jet-Engines, 2018, v. 35, n. 4, p. 321, doi. 10.1515/tjj-2015-0014

By:

Shi, Deyong;
Song, Wenyan;
Ye, Jingfeng;
Tao, Bo;
Wang, Yanhua;
Fu, Qiang

Publication type:

Article