Michael Oschwald - Publications, H-index & Citations

Michael Oschwald

helmholtz association

25H指数

368论文数

3.1K被引数

收录论文 15

发表时间

Optimized Postprocessing Method for Fatigue Life Evaluation of Reusable Rocket Combustion Chambers 用于可重复使用火箭燃烧室疲劳寿命评估的优化后处理方法

Journal of Propulsion and Power

IF2.4

2025-10-01

PREAI

Gulczynski, Mateusz T.; Riccius, Jorg; Deeken, Jan C.; Oschwald, Michael

Heat Transport Processes of Gaseous Film Cooling in Rocket Combustion Chambers

JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER

IF1.7

2025-10-01

PREAI

Kuhlwein, Georg; Suslov, Dmitry; Oschwald, Michael

Influence of Injector and Chamber Design on LOX/CH4 Combustion Instabilities 喷嘴和燃烧室设计对LOX/CH4燃烧不稳定性的影响

JOURNAL OF PROPULSION AND POWER

IF2.4

2025-09-01

PREAI

Martin, Jan; Armbruster, Wolfgang; Borner, Michael; Hardi, Justin; Nakaya, Shinji; Oschwald, Michael

Obtaining pseudo-OH * radiation images from CFD solutions of transcritical flames

COMBUSTION AND FLAME

IF6.2

2021-11-01

OAAI

Tonti, Federica; Perovsek, Jaka; Usandivaras, Jose' Zapata; Karl, Sebastian; Hardi, Justin S.; Morii, Youhi; Oschwald, Michael

Dense core response to forced acoustic fields in oxygen-hydrogen rocket flames

PROPULSION AND POWER RESEARCH

IF6.3

2020-09-01

OAAI

Morii, Youhi; Beinke, Scott; Hardi, Justin; Shimizu, Taro; Kawashima, Hideto; Oschwald, Michael

Numerical and experimental analysis of flashing cryogenic nitrogen

INTERNATIONAL JOURNAL OF MULTIPHASE FLOW

IF3.8

2020-09-01

PREAI

Gaertner, Jan Wilhelm; Kronenburg, Andreas; Rees, Andreas; Sender, Joachim; Oschwald, Michael; Lamanna, Grazia

Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines

ACTA ASTRONAUTICA

IF3.4

2020-04-01

OAAI

Armbruster, Wolfgang; Hardi, Justin S.; Miene, Yannik; Suslov, Dmitry; Oschwald, Michael

Full-length visualisation of liquid oxygen disintegration in a single injector sub-scale rocket combustor

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2019-03-01

OAAI

Suslov, Dmitry I.; Hardi, Justin S.; Oschwald, Michael

Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor

ACTA ASTRONAUTICA

IF3.4

2018-10-01

PREAI

Armbruster, Wolfgang; Hardi, Justin S.; Suslov, Dmitry; Oschwald, Michael

Combustion dynamics in cryogenic rocket engines: Research programme at DLR Lampoldshausen

ACTA ASTRONAUTICA

IF3.4

2018-06-01

PREAI

Hardi, Justin S.; Traudt, Tobias; Bombardieri, Cristiano; Boerner, Michael; Beinke, Scott K.; Armbruster, Wolfgang; Blanco, P. Nicolas; Tonti, Federica; Suslov, Dmitry; Dally, Bassam; Oschwald, Michael

Measurement of acoustic dissipation in an experimental combustor under representative conditions

JOURNAL OF SOUND AND VIBRATION

IF4.9

2017-03-01

PREAI

Webster, Samuel; Hardi, Justin; Oschwald, Michael

Large eddy simulation of laser ignition and compressible reacting flow in a rocket-like configuration

COMBUSTION AND FLAME

IF6.2

2009-06-01

OAAI

Lacaze, G.; Cuenot, B.; Poinsot, T.; Oschwald, M.

Steady-state high pressure LOx/H2 rocket engine combustion

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2007-01-01

OAAI

Smith, Joshua J.; Schneider, Gerald; Suslov, Dmitry; Oschwald, Michael; Haidn, Oskar

Ignition of cryogenic H2/LOX sprays

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2003-10-01

PREAI

Gurliat, O; Schmidt, V; Haidn, OJ; Oschwald, M

Temperature measurements by coherent anti-Stokes Raman spectroscopy in hydrogen-fuelled scramjet combustor

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2001-07-01

PREAI

Vereschagin, KA; Smirnov, VV; Stelmakh, OM; Fabelinsky, VI; Sabelnikov, VA; Ivanov, VV; Clauss, W; Oschwald, M

研究方向