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Output details

15 - General Engineering

University of Oxford

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Output 80 of 354 in the submission
Article title

Comparison of Mach 10 Scramjet Data From Different Impulse Facilities

Type
D - Journal article
Title of journal
AIAA Journal: devoted to aerospace research and development
Article number
-
Volume number
48
Issue number
8
First page of article
1635
ISSN of journal
0001-1452
Year of publication
2010
URL
-
Number of additional authors
1
Additional information

This paper verifies the first use of an expansion tube to ground test a full scramjet, which is the only viable facility for above Mach 10 testing. It led to the funding and development of nozzles to allow future testing of full-scale flight experiments in the X3 facility at the University of Queensland. The research directly supported two successful grant applications to investigate Mach12 and 15 scramjets in the X3 expansion tube facility, specifically, the Australian Research Council discovery grant “The Science of Scramjet Propulsion DP130102617” for $AU550K and Scramspace totalling $AU15M including $AU1M for expansion tube development (details available).

Interdisciplinary
-
Cross-referral requested
-
Research group
G - Thermodynamics and Fluids
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-