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Non-equilibrium viscous shock-layer technique for computing hypersonic flow around blunt-nosed slender bodies

Authors: Ghasemloo, S.; Mani, M.

Source: International Journal of Numerical Methods for Heat & Fluid Flow, Volume 19, Number 5, 2009 , pp. 574-594(21)

Publisher: Emerald Group Publishing Limited

Effects of boundary-layers bleeding on performance parameters of hypersonic inlets

Authors: Chang, Juntao; Fan, Yi

Source: Aircraft Engineering and Aerospace Technology: An International Journal, Volume 81, Number 3, 2009 , pp. 204-211(8)

Publisher: Emerald Group Publishing Limited

Full Text

Author: Brun, Raymond

Source: Introduction to Reactive Gas Dynamics, February 2009 , pp. i-408(409)

Publisher: Oxford Scholarship Online Monographs

Part 1. Fundamental Statistical Aspects

Author: Brun, Raymond

Source: Introduction to Reactive Gas Dynamics, February 2009 , pp. 1-3(3)

Publisher: Oxford Scholarship Online Monographs

Notations to Part I

Author: Brun, Raymond

Source: Introduction to Reactive Gas Dynamics, February 2009 , pp. 3-5(3)

Publisher: Oxford Scholarship Online Monographs

Part II. Macroscopic Aspects and Applications

Author: Brun, Raymond

Source: Introduction to Reactive Gas Dynamics, February 2009 , pp. 189-191(3)

Publisher: Oxford Scholarship Online Monographs

Notations to Part II

Author: Brun, Raymond

Source: Introduction to Reactive Gas Dynamics, February 2009 , pp. 191-195(5)

Publisher: Oxford Scholarship Online Monographs

Ten. Reactive Flows in the Dissipative Regime

Author: Brun, Raymond

Source: Introduction to Reactive Gas Dynamics, February 2009 , pp. 294-326(33)

Publisher: Oxford Scholarship Online Monographs

Aerodynamic force measurement using 3-component accelerometer force balance system in a hypersonic shock tunnel

Authors: Saravanan, S.; Jagadeesh, G.; Reddy, K.

Source: Shock Waves, Volume 18, Number 6, February 2009 , pp. 425-435(11)

Publisher: Springer

Numerical simulation of air&#47;H<SUB align=right>2 combustion processes in a scramjet turbulent flow

Authors: Burtschell, Y.; Seror, S.; Parisse, J.D.; Zeitoun, D.

Source: Progress in Computational Fluid Dynamics, An International Journal, Volume 8, Number 6, 18 August 2008 , pp. 320-330(11)

Publisher: Inderscience Publishers

Using axisymmetric analogue along the streamlines for the solution of three-dimensional viscous shock layer equations of hypersonic equilibrium flow

Authors: Noori, S.; Karimian, S. M. H.

Source: International Journal of Computational Fluid Dynamics, Volume 22, Number 6, July 2008 , pp. 429-436(8)

Publisher: Taylor and Francis Ltd

Optimum Design of Cross-Flow Shell and Tube Heat Exchangers with Low Fin Tubes

Authors: Benarji, N.; Balaji, C.; Venkateshan, S. P.

Source: Heat Transfer Engineering, Volume 29, Number 10, October 2008 , pp. 864-872(9)

Publisher: Taylor and Francis Ltd

Computation of non-equilibrium hypersonic flow with artificially upstream flux vector splitting (AUFS) schemes

Authors: Tchuen, Ghislain; Burtschell, Yves; Zeitoun, David

Source: International Journal of Computational Fluid Dynamics, Volume 22, Number 4, April 2008 , pp. 209-220(12)

Publisher: Taylor and Francis Ltd

Wavelet Cross-Spectrum Analysis of Multi-Scale Disturbance Instability and Transition on Sharp Cone Hypersonic Boundary Layer

Authors: Jian, Han; Nan, Jiang

Source: Chinese Physics Letters, Volume 25, Number 5, May 2008 , pp. 1731-1733(3)

Publisher: Institute of Physics Publishing

Acoustic receptivity of Mach 4.5 boundary layer with leading-edge bluntness

Authors: Malik, M.; Balakumar, P.

Source: Theoretical and Computational Fluid Dynamics, Volume 21, Number 5, September 2007 , pp. 323-342(20)

Publisher: Springer

Re-entry body drag: shock tunnel experiments and computational fluid dynamics calculations compared

Authors: Boyce, Russell; Stumvoll, Alexander

Source: Shock Waves, Volume 16, Number 6, July 2007 , pp. 431-443(13)

Publisher: Springer

Three-dimensional effects on line-of-sight visualization measurements of supersonic and hypersonic flow over cylinders

Authors: Eichmann, Troy; McIntyre, Timothy; Bishop, Alexis; Vakata, Sosefo; Rubinsztein-Dunlop, Halina

Source: Shock Waves, Volume 16, Numbers 4-5, May 2007 , pp. 299-307(9)

Publisher: Springer

Study of the aerodynamic stability of a blunt cone with a side flap in a hypersonic flow

Authors: Krasil'nikov, A.; Mordvintsev, G.; Shmanenkov, V.

Source: Fluid Dynamics, Volume 42, Number 1, January 2007 , pp. 107-114(8)

Publisher: Springer

Laminar-turbulent transition in the boundary layer on cones in a hypersonic flow at high Reynolds numbers per meter

Authors: Vasil'ev, A.; Rychkov, V.; Topchiyan, M.

Source: Journal of Applied Mechanics and Technical Physics, Volume 48, Number 3, May 2007 , pp. 361-367(7)

Publisher: Springer

Stability analysis and transition prediction of hypersonic boundary layer over a blunt cone with small nose bluntness at zero angle of attack

Authors: Su, Cai-hong; Zhou, Heng

Source: Applied Mathematics and Mechanics, Volume 28, Number 5, May 2007 , pp. 563-572(10)

Publisher: Springer