Effects of Shock-Tube Cleanliness on Slender-Body Hypersonic Instability and Transition Studies at High-Enthalpy

Parziale, Nick J.; Jewell, Joseph S.; Leyva, Ivett A.; Shepherd, Joseph E.

doi:10.2514/6.2015-1786

53rd AIAA Aerospace Sciences Meeting 2015

DOI: 10.2514/6.2015-1786

|View full text |Cite

Effects of Shock-Tube Cleanliness on Slender-Body Hypersonic Instability and Transition Studies at High-Enthalpy

Nick J. Parziale

Joseph S. Jewell

Ivett A. Leyva

et al.

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

Supporting

Mentioning

Contrasting

Year Published

2016

2021

Publication Types

Select...

Other4

Relationship

Self Cite1

Independent3

Authors

Journals

Cited by 4 publications

References 44 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

Boundary Layer Stability Analysis for Stetson’s Mach 6 Blunt Cone Experiments

Jewell

Kimmel

2016

54th AIAA Aerospace Sciences Meeting

Self Cite

View full text Add to dashboard Cite

The results of a seminal experimental study of the effects of bluntness and swallowing length on transition on an 8-degree cone at zero angle of attack in Mach 6 high Reynolds number flow are analyzed with the STABL computational fluid dynamics code package. Mean flow solutions and PSE-Chem stability analyses for a total of 11 different nose tip bluntnesses, ranging from sharp to 15.24 mm radius, are obtained. For the sharpest cases, N Tr ≈ 7, but as bluntness increases and the calculated swallowing distance lengthens, the computed N-factor at the experimentally-observed transition location drops below the level at which Mack's second mode would be expected to lead to transition. These results indicate that the dominant instability mechanism for the bluntest cases is not the second mode.

show abstract

Boundary Layer Stability Analysis for Stetson’s Mach 6 Blunt Cone Experiments

Jewell

Kimmel

2016

54th AIAA Aerospace Sciences Meeting

Self Cite

View full text Add to dashboard Cite

show abstract

Focused Laser Differential Interferometry Measurements at NASA Langley 20-Inch Mach 6

Weisberger

Bathel

Jones

et al. 2019

AIAA Aviation 2019 Forum

View full text Add to dashboard Cite

Analysis of the Amplitude Response of a Two-Point and a Multi-Point Focused Laser Differential Interferometer

Bathel

Weisberger

Herring

et al. 2021

AIAA Scitech 2021 Forum

View full text Add to dashboard Cite

scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.

Contact Info

customersupport@researchsolutions.com

10624 S. Eastern Ave., Ste. A-614

Henderson, NV 89052, USA

This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.

Blog Terms and Conditions API Terms Privacy Policy Contact Cookie Preferences Do Not Sell or Share My Personal Information

Made with 💙 for researchers

Part of the Research Solutions Family.

Effects of Shock-Tube Cleanliness on Slender-Body Hypersonic Instability and Transition Studies at High-Enthalpy

Cited by 4 publications

References 44 publications

Boundary Layer Stability Analysis for Stetson’s Mach 6 Blunt Cone Experiments

Boundary Layer Stability Analysis for Stetson’s Mach 6 Blunt Cone Experiments

Focused Laser Differential Interferometry Measurements at NASA Langley 20-Inch Mach 6

Analysis of the Amplitude Response of a Two-Point and a Multi-Point Focused Laser Differential Interferometer

Contact Info

Product

Resources

About