Hybrid problems of determining unknown shape of bladings in compressible S2-flow in mixed-flow turbomachinery via variational technique

Author： He Ji-Huan  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.71, Iss.2, 1999-02, pp. : 154-159

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

Inverse problems of determining the unknown shape of oscillating airfoils in compressible 2D unsteady flow via variational technique

By He Ji-Huan  

Aircraft Engineering, Vol. 72, Iss. 1, 2000-01 ,pp. : 18-24

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Design optimization of a mixed-flow compressor impeller for a small turbojet engine

By Cevik Mert   Uzol Oguz  

Aircraft Engineering, Vol. 83, Iss. 3, 2011-05 ,pp. : 127-137

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Quick Graphical Methods in Compressible Flow Problems: A Chart for the Solution of a Number of Common High-Speed Flow Problems

By Rabineau B.  

Aircraft Engineering, Vol. 29, Iss. 2, 1993-12 ,pp. : 39-43

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Compressible Flow Behind a Wing

By Husk D.I.  

Aircraft Engineering, Vol. 14, Iss. 6, 1993-12 ,pp. : 160-160

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Flow of a Compressible Gas with Friction: A Study of the Effects of Friction in Compressible Flow and the Development of a Correction Factor

By Naylor V.D.  

Aircraft Engineering, Vol. 23, Iss. 10, 1993-12 ,pp. : 308-310

Emerald Group Publishing Ltd

Access to resources Recommend Favorite