NDLI: Interaction theory of hypersonic laminar near-wake flow behind an adiabatic circular cylinder

Content Provider	Springer Nature Link
Author	Hinman, W. Schuyler Johansen, C. T.
Copyright Year	2015
Abstract	The separation and shock wave formation on the aft-body of a hypersonic adiabatic circular cylinder were studied numerically using the open source software OpenFOAM. The simulations of laminar flow were performed over a range of Reynolds numbers ( $$8\times 10^3 < Re < 8\times 10^4$$ ) at a free-stream Mach number of 5.9. Off-body viscous forces were isolated by controlling the wall boundary condition. It was observed that the off-body viscous forces play a dominant role compared to the boundary layer in displacement of the interaction onset in response to a change in Reynolds number. A modified free-interaction equation and correlation parameter has been presented which accounts for wall curvature effects on the interaction. The free-interaction equation was manipulated to isolate the contribution of the viscous–inviscid interaction to the overall pressure rise and shock formation. Using these equations coupled with high-quality simulation data, the underlying mechanisms resulting in Reynolds number dependence of the lip-shock formation were investigated. A constant value for the interaction parameter representing the part of the pressure rise due to viscous–inviscid interaction has been observed at separation over a wide range of Reynolds numbers. The effect of curvature has been shown to be the primary contributor to the Reynolds number dependence of the free-interaction mechanism at separation. The observations in this work have been discussed here to create a thorough analysis of the Reynolds number-dependent nature of the lip-shock.
Starting Page	717
Ending Page	727
Page Count	11
File Format	PDF
ISSN	09381287
Journal	Shock Waves
Volume Number	26
Issue Number	6
e-ISSN	14322153
Language	English
Publisher	Springer Berlin Heidelberg
Publisher Date	2015-12-30
Publisher Place	Berlin, Heidelberg
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Interaction theory Hypersonic laminar near-wake Computational fluid dynamics Lip separation shock Viscous–inviscid interaction Engineering Thermodynamics, Heat and Mass Transfer Fluid- and Aerodynamics Engineering Fluid Dynamics Thermodynamics Acoustics Condensed Matter Physics
Content Type	Text
Resource Type	Article
Subject	Physics and Astronomy Mechanical Engineering

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

Interaction theory of hypersonic laminar near-wake flow behind an adiabatic circular cylinder

Laminar vortex shedding behind a cooled circular cylinder

Hysteresis phenomenon at interaction of shock waves generated by a cylinder array

Shock wave induced by a high-intensity power source in hypersonic flow

Effect of viscosity and wall heat conduction on shock attenuation in narrow channels

On energy focusing with multiple sources in an inviscid field

Unsteady flow with separation behind a shock wave diffracting over curved walls

Laminar near wake of a sharp wedge in hypersonic perfect-gas flow

Experiments in hand-operated, hypersonic shock tunnel facility

Interaction theory of hypersonic laminar near-wake flow behind an adiabatic circular cylinder

Similar Documents

Interaction theory of hypersonic laminar near-wake flow behind an adiabatic circular cylinder

Laminar vortex shedding behind a cooled circular cylinder

Hysteresis phenomenon at interaction of shock waves generated by a cylinder array

Shock wave induced by a high-intensity power source in hypersonic flow

Effect of viscosity and wall heat conduction on shock attenuation in narrow channels

On energy focusing with multiple sources in an inviscid field

Unsteady flow with separation behind a shock wave diffracting over curved walls

Laminar near wake of a sharp wedge in hypersonic perfect-gas flow

Experiments in hand-operated, hypersonic shock tunnel facility

Interaction theory of hypersonic laminar near-wake flow behind an adiabatic circular cylinder