9th International Space Planes and Hypersonic Systems and Technologies Conference 1999
DOI: 10.2514/6.1999-4915
|View full text |Cite
|
Sign up to set email alerts
|

Experimental investigation of inclined hydrogen injection into a supersonic flow

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
5

Citation Types

0
6
0

Year Published

2004
2004
2018
2018

Publication Types

Select...
4
1

Relationship

2
3

Authors

Journals

citations
Cited by 10 publications
(6 citation statements)
references
References 7 publications
0
6
0
Order By: Relevance
“…3,7,[11][12][13][14][15][16][17] We used it to investigate the timeaveraged mixing conditions of the 2-D hydrogen-air supersonic mixing layer in previous studies. 15,16) We clarified that…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…3,7,[11][12][13][14][15][16][17] We used it to investigate the timeaveraged mixing conditions of the 2-D hydrogen-air supersonic mixing layer in previous studies. 15,16) We clarified that…”
Section: Introductionmentioning
confidence: 99%
“…For example, the freestream remains supersonic in the combustor, so mixing of fuel jets with the freestream must be quick. Some injection schemes to enhance the mixing for the SCRAMJET have been suggested, [2][3][4][5][6][7][8][9][10][11] such as wedge shaped injector schemes 2,3) and their derivations, 4,5) rampinjector schemes 6,7) and their derivations 8,9) and inclined-injector schemes. 10,11) It is important to evaluate the mixing condition in the SCRAMJET in order to suggest or develop these injection schemes.…”
Section: Introductionmentioning
confidence: 99%
“…[2][3][4][5][6][7][8][9] For example, a ramp injector is one of the schemes to enhance mixing by using induced vorticity. [2][3][4] An inclined injection scheme was suggested to reduce the total pressure loss of the freestream.…”
Section: Introductionmentioning
confidence: 99%
“…[2][3][4] An inclined injection scheme was suggested to reduce the total pressure loss of the freestream. 5,6) Meanwhile, a wedge shaped injector [7][8][9] was developed to minimize both total pressure loss and jet-boundary layer interaction. Regarding investigations about wedge injectors, as far as we know, gaseous hydrogen has not been used as the injectant in the previous studies.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation