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

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Uzay Mühendisliği Bölümü

Araştırma sonucu: Dergiye katkı › İnceleme makalesi › bilirkişi

83 Atıf (Scopus)

Özet

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.

Orijinal dil	İngilizce
Sayfa (başlangıç-bitiş)	39-53
Sayfa sayısı	15
Dergi	Progress in Aerospace Sciences
Hacim	90
DOI'lar	https://doi.org/10.1016/j.paerosci.2017.02.001
Yayın durumu	Yayınlandı - Nis 2017

Bibliyografik not

Publisher Copyright:
© 2017 Elsevier Ltd

Belgeye Erişim

10.1016/j.paerosci.2017.02.001

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

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, hac. 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

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