High order numerical simulation of the thermal load on a lobed strut injector for scramjet applications

Author:

Simsont Yann Hendrik1,Gerlinger Peter1

Affiliation:

1. Institut für Verbrennungstechnik der Luft‐ und Raumfahrt Universität Stuttgart Pfaffenwaldring 38‐40 70569 Stuttgart Germany

Funder

Deutsche Forschungsgemeinschaft

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference46 articles.

1. KoderaM SunamiT ItohK.Numerical simulation of a scramjet engine for JAXAs flight experiment using hyshot.AIAA 2005‐3335 Capua Italy 2005;1–11.

2. SchrammJM KarlS HannemannK SteelantJ.Ground testing of the hyshot II scramjet configuration in HEG.AIAA 2008‐2547 Glasgow Scotland 2008;1–12.

3. SmartMK SuraweeraMV.HIFiRE 7 – development of a 3d scramjet for flight testing.AIAA 2009‐7259 Bremen Germany 2009;1–20.

4. Investigation of a contoured wall injector for hypervelocity mixing augmentation

5. BaurleR FullerR WhiteJ ChenT GruberM NejadA.An investigation of advanced fuel injection schemes for scramjet combustion.AIAA 98‐0937 Reno NV USA 1998;1–14.

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