Minimum forebody drag in hypersonic continuum and rarefied flows

E-ISSN： 2059-6464|110|1108|369-374

ISSN： 0001-9240

Source： The Aeronautical Journal, Vol.110, Iss.1108, 2006-06, pp. : 369-374

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Hypersonic minimum drag forebodies with blunt leading edges

The Aeronautical Journal, Vol. 117, Iss. 1191, 2013-05 ,pp. : 553-557

Cambridge University Press

Access to resources Recommend Favorite

Rarefied, superorbital flows in an expansion tube

By Wheatley V Chiu H.S. Jacobs P.A. Macrossan M.N. Mee D.J. Morgan R.G.

International Journal of Numerical Methods for Heat & Fluid Flow, Vol. 14, Iss. 4, 2004-04 ,pp. : 512-537

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Drag reduction on a spiked body at hypersonic speed

The Aeronautical Journal, Vol. 114, Iss. 1152, 2010-02 ,pp. : 113-119

Cambridge University Press

Access to resources Recommend Favorite

Computational study of drag increase due to wall roughness for hypersonic flight

The Aeronautical Journal, Vol. 121, Iss. 1237, 2017-03 ,pp. : 395-415

Cambridge University Press

Access to resources Recommend Favorite

Experimental and computational study of unsteady hypersonic cavity flows

The Aeronautical Journal, Vol. 111, Iss. 1125, 2007-11 ,pp. : 673-688

Cambridge University Press

Access to resources Recommend Favorite