Testing of DLR C/C-SiC and C/C for HIFiRE 8 Scramjet Combustor-Reference-Cited by-同舟云学术

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Testing of DLR C/C-SiC and C/C for HIFiRE 8 Scramjet Combustor

Published:2014-06-13 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
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Author:

Glass David E.¹,Capriotti Diego¹,Reimer Thomas²,Kütemeyer Marius²,Smart Michael³

Affiliation:

1. NASA Langley Research Center

2. German Aerospace Center (DLR)

3. University of Queensland

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3089

Reference4 articles.

1. Study of Boundary-Layer Transition on Hypersonic International Flight Research Experimentation 5

2. Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment

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1. Materials, Structures, and Thermal Management;Scramjet Propulsion;2022-11-18

2. Preliminary Analysis of the Hexafly-International Vehicle;Aerotecnica Missili & Spazio;2018-07

3. Composite materials used in Scramjet- A Review;Materials Today: Proceedings;2018

4. SiCnw/PyC core-shell networks to improve the bonding strength and oxyacetylene ablation resistance of ZrB2–ZrC coating for C/C–ZrB2–ZrC–SiC composites;Carbon;2017-11

5. Octra - Optimized Ceramic for Hypersonic Application with Transpiration Cooling;Ceramic Transactions Series;2017-07-14

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