Assessment of predictive capabilities for aerodynamic heating in hypersonic flow

Doyle Knight; Olivier Chazot; Joanna Austin; Mohammad Ali Badr; Graham Candler; Bayram Celik; Donato de Rosa; Raffaele Donelli; Jeffrey Komives; Andrea Lani; Deborah Levin; Ioannis Nompelis; Marco Panesi; Giuseppe Pezzella; Bodo Reimann; Ozgur Tumuklu; Kemal Yuceil

doi:10.1016/j.paerosci.2017.02.001

Assessment of predictive capabilities for aerodynamic heating in hypersonic flow

Doyle Knight^*, Olivier Chazot, Joanna Austin, Mohammad Ali Badr, Graham Candler, Bayram Celik, Donato de Rosa, Raffaele Donelli, Jeffrey Komives, Andrea Lani, Deborah Levin, Ioannis Nompelis, Marco Panesi, Giuseppe Pezzella, Bodo Reimann, Ozgur Tumuklu, Kemal Yuceil

^*Corresponding author for this work

Department of Astronautical Engineering

Research output: Contribution to journal › Review article › peer-review

79 Citations (Scopus)

Abstract

The capability for CFD prediction of hypersonic shock wave laminar boundary layer interaction was assessed for a double wedge model at Mach 7.1 in air and nitrogen at 2.1 MJ/kg and 8 MJ/kg. Simulations were performed by seven research organizations encompassing both Navier-Stokes and Direct Simulation Monte Carlo (DSMC) methods as part of the NATO STO AVT Task Group 205 activity. Comparison of the CFD simulations with experimental heat transfer and schlieren visualization suggest the need for accurate modeling of the tunnel startup process in short-duration hypersonic test facilities, and the importance of fully 3-D simulations of nominally 2-D (i.e., non-axisymmmetric) experimental geometries.

Original language	English
Pages (from-to)	39-53
Number of pages	15
Journal	Progress in Aerospace Sciences
Volume	90
DOIs	https://doi.org/10.1016/j.paerosci.2017.02.001
Publication status	Published - Apr 2017

Bibliographical note

Publisher Copyright:
© 2017 Elsevier Ltd

Keywords

CFD
Heat transfer
Hypersonic

Access to Document

10.1016/j.paerosci.2017.02.001

Cite this

Knight, D., Chazot, O., Austin, J., Badr, M. A., Candler, G., Celik, B., Rosa, D. D., Donelli, R., Komives, J., Lani, A., Levin, D., Nompelis, I., Panesi, M., Pezzella, G., Reimann, B., Tumuklu, O., & Yuceil, K. (2017). Assessment of predictive capabilities for aerodynamic heating in hypersonic flow. Progress in Aerospace Sciences, 90, 39-53. https://doi.org/10.1016/j.paerosci.2017.02.001

@article{8e2fe269ef104f959ec9195b15a790c2,

title = "Assessment of predictive capabilities for aerodynamic heating in hypersonic flow",

abstract = "The capability for CFD prediction of hypersonic shock wave laminar boundary layer interaction was assessed for a double wedge model at Mach 7.1 in air and nitrogen at 2.1 MJ/kg and 8 MJ/kg. Simulations were performed by seven research organizations encompassing both Navier-Stokes and Direct Simulation Monte Carlo (DSMC) methods as part of the NATO STO AVT Task Group 205 activity. Comparison of the CFD simulations with experimental heat transfer and schlieren visualization suggest the need for accurate modeling of the tunnel startup process in short-duration hypersonic test facilities, and the importance of fully 3-D simulations of nominally 2-D (i.e., non-axisymmmetric) experimental geometries.",

keywords = "CFD, Heat transfer, Hypersonic",

author = "Doyle Knight and Olivier Chazot and Joanna Austin and Badr, {Mohammad Ali} and Graham Candler and Bayram Celik and Rosa, {Donato de} and Raffaele Donelli and Jeffrey Komives and Andrea Lani and Deborah Levin and Ioannis Nompelis and Marco Panesi and Giuseppe Pezzella and Bodo Reimann and Ozgur Tumuklu and Kemal Yuceil",

note = "Publisher Copyright: {\textcopyright} 2017 Elsevier Ltd",

year = "2017",

month = apr,

doi = "10.1016/j.paerosci.2017.02.001",

language = "English",

volume = "90",

pages = "39--53",

journal = "Progress in Aerospace Sciences",

issn = "0376-0421",

publisher = "Elsevier Ltd",

}

Knight, D, Chazot, O, Austin, J, Badr, MA, Candler, G, Celik, B, Rosa, DD, Donelli, R, Komives, J, Lani, A, Levin, D, Nompelis, I, Panesi, M, Pezzella, G, Reimann, B, Tumuklu, O & Yuceil, K 2017, 'Assessment of predictive capabilities for aerodynamic heating in hypersonic flow', Progress in Aerospace Sciences, vol. 90, pp. 39-53. https://doi.org/10.1016/j.paerosci.2017.02.001

TY - JOUR

T1 - Assessment of predictive capabilities for aerodynamic heating in hypersonic flow

AU - Knight, Doyle

AU - Chazot, Olivier

AU - Austin, Joanna

AU - Badr, Mohammad Ali

AU - Candler, Graham

AU - Celik, Bayram

AU - Rosa, Donato de

AU - Donelli, Raffaele

AU - Komives, Jeffrey

AU - Lani, Andrea

AU - Levin, Deborah

AU - Nompelis, Ioannis

AU - Panesi, Marco

AU - Pezzella, Giuseppe

AU - Reimann, Bodo

AU - Tumuklu, Ozgur

AU - Yuceil, Kemal

PY - 2017/4

Y1 - 2017/4

N2 - The capability for CFD prediction of hypersonic shock wave laminar boundary layer interaction was assessed for a double wedge model at Mach 7.1 in air and nitrogen at 2.1 MJ/kg and 8 MJ/kg. Simulations were performed by seven research organizations encompassing both Navier-Stokes and Direct Simulation Monte Carlo (DSMC) methods as part of the NATO STO AVT Task Group 205 activity. Comparison of the CFD simulations with experimental heat transfer and schlieren visualization suggest the need for accurate modeling of the tunnel startup process in short-duration hypersonic test facilities, and the importance of fully 3-D simulations of nominally 2-D (i.e., non-axisymmmetric) experimental geometries.

AB - The capability for CFD prediction of hypersonic shock wave laminar boundary layer interaction was assessed for a double wedge model at Mach 7.1 in air and nitrogen at 2.1 MJ/kg and 8 MJ/kg. Simulations were performed by seven research organizations encompassing both Navier-Stokes and Direct Simulation Monte Carlo (DSMC) methods as part of the NATO STO AVT Task Group 205 activity. Comparison of the CFD simulations with experimental heat transfer and schlieren visualization suggest the need for accurate modeling of the tunnel startup process in short-duration hypersonic test facilities, and the importance of fully 3-D simulations of nominally 2-D (i.e., non-axisymmmetric) experimental geometries.

KW - CFD

KW - Heat transfer

KW - Hypersonic

UR - http://www.scopus.com/inward/record.url?scp=85011999914&partnerID=8YFLogxK

U2 - 10.1016/j.paerosci.2017.02.001

DO - 10.1016/j.paerosci.2017.02.001

M3 - Review article

AN - SCOPUS:85011999914

SN - 0376-0421

VL - 90

SP - 39

EP - 53

JO - Progress in Aerospace Sciences

JF - Progress in Aerospace Sciences

ER -

Assessment of predictive capabilities for aerodynamic heating in hypersonic flow

Abstract

Bibliographical note

Keywords

Access to Document

Other files and links

Fingerprint

Cite this