18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012
DOI: 10.2514/6.2012-5889
|View full text |Cite
|
Sign up to set email alerts
|

Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustion

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

3
12
0

Year Published

2015
2015
2017
2017

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 7 publications
(15 citation statements)
references
References 24 publications
3
12
0
Order By: Relevance
“…The influence of shock tube fill pressure and temperature uncertainties were found to be negligible, and so will not be considered here. Their minimal influence is clearly apparent in the low sensitivity values in These values are similar to those stated in [59,63,66]. Further justification of these values are given here:…”
Section: C2 Uncertainties In Measured Quantitiessupporting
confidence: 74%
See 4 more Smart Citations
“…The influence of shock tube fill pressure and temperature uncertainties were found to be negligible, and so will not be considered here. Their minimal influence is clearly apparent in the low sensitivity values in These values are similar to those stated in [59,63,66]. Further justification of these values are given here:…”
Section: C2 Uncertainties In Measured Quantitiessupporting
confidence: 74%
“…The uncertainty of which is conservatively estimated as X P SR = X 2 P ,Stag + X 2 P ,Pitot . X P ,Pitot was taken from [59,66] as 8.8 %.…”
Section: C2 Uncertainties In Measured Quantitiesmentioning
confidence: 99%
See 3 more Smart Citations