Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
1991.
Chemical reactions in high-speed flows.
Philosophical Transactions of the Royal Society of London. Series A: Physical and Engineering Sciences,
Vol. 335,
Issue. 1637,
p.
161.
Gai, S.L.
1992.
Free piston shock tunnels: developments and capabilities.
Progress in Aerospace Sciences,
Vol. 29,
Issue. 1,
p.
1.
Reddy, N M
Nagashetty, K
Jagadeesh, G
and
Reddy, K P J
1996.
Review of hypersonic research investigations in IISc shock tunnel (HST1).
Sadhana,
Vol. 21,
Issue. 6,
p.
741.
Macrossan, M. N.
and
Eckett, C.
1996.
Chemical nonequilibrium inviscid flow over a blunt cone at incidence.
AIAA Journal,
Vol. 34,
Issue. 10,
p.
2054.
Park, Chul
1996.
Experimental evaluation of real-gas phenomena in high enthalpy impulse test facilities - A review.
2002.
Advanced Hypersonic Test Facilities.
p.
17.
Sahoo, Niranjan
Mahapatra, D R
Jagadeesh, G
Gopalakrishnan, S
and
Reddy, K P J
2003.
An accelerometer balance system for measurement of aerodynamic force coefficients over blunt bodies in a hypersonic shock tunnel.
Measurement Science and Technology,
Vol. 14,
Issue. 3,
p.
260.
Capra, Bianca
and
Morgan, Richard
2006.
Radiative and Total Heat Transfer Measurements to a Titan Explorer Model.
Roy, Christopher J.
and
Blottner, Frederick G.
2006.
Review and assessment of turbulence models for hypersonic flows.
Progress in Aerospace Sciences,
Vol. 42,
Issue. 7-8,
p.
469.
Mundt, Christian
Boyce, Russell
Jacobs, Peter
and
Hannemann, Klaus
2007.
Validation study of numerical simulations by comparison to measurements in piston-driven shock-tunnels.
Aerospace Science and Technology,
Vol. 11,
Issue. 2-3,
p.
100.
Schemperg, K.
and
Mundt, C.
2009.
Shock Waves.
p.
477.
Wen, Chihyung
and
Hornung, Hans
2010.
Nonequilibrium recombination after a curved shock wave.
Progress in Aerospace Sciences,
Vol. 46,
Issue. 2-3,
p.
132.
Kirchhartz, Rainer M.
Mee, David J.
Stalker, Raymond J.
Jacobs, Peter A.
and
Smart, Michael K.
2010.
Supersonic Boundary-Layer Combustion: Effects of Upstream Entropy and Shear-Layer Thickness.
Journal of Propulsion and Power,
Vol. 26,
Issue. 1,
p.
57.
Tanimizu, Katsuyoshi
Mee, David J.
Stalker, Raymond J.
and
Jacobs, Peter A.
2011.
Thrust Nozzle Design Study for a Quasi-Axisymmetric Scramjet-Powered Vehicle.
Journal of Propulsion and Power,
Vol. 27,
Issue. 1,
p.
40.
Gildfind, D. E.
Morgan, R. G.
McGilvray, M.
Jacobs, P. A.
Stalker, R. J.
and
Eichmann, T. N.
2011.
Free-piston driver optimisation for simulation of high Mach number scramjet flow conditions.
Shock Waves,
Vol. 21,
Issue. 6,
p.
559.
Jacobs, C.
Morgan, R.
McIntyre, T.
and
Laux, C.
2012.
Radiative heat transfer measurements in low density Titan atmospheres.
Gildfind, David
Morgan, Richard
McGilvray, Mathew
and
Jacobs, Peter
2012.
Simulation of High Mach Number Scramjet Flow Conditions using the X2 Expansion Tube.
Gildfind, D. E.
Morgan, R. G.
McGilvray, M.
and
Jacobs, P. A.
2012.
28th International Symposium on Shock Waves.
p.
273.
Tanimizu, Katsuyoshi
Mee, David J.
Stalker, Raymond J.
and
Jacobs, Peter A.
2013.
Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions.
Shock Waves,
Vol. 23,
Issue. 5,
p.
453.
de Crombrugghe, G.
Morgan, R.
and
Chazot, O.
2016.
Theoretical approach and experimental verification of the role of diffusive transport under binary scaling conditions.
International Journal of Heat and Mass Transfer,
Vol. 97,
Issue. ,
p.
675.