Re´sume´ of Compressor Research at the NACA Langley Laboratory

Author:

Savage M.1,Boxer E.1,Erwin J. R.2

Affiliation:

1. NASA, Langley Laboratory, Virginia

2. General Electric Company

Abstract

This paper describes the compressor research program conducted at the NACA Langley Laboratory and highlights the significant developments obtained prior to the discontinuance of this program in 1957. Results of low speed, high speed, and transonic cascade testing are noted. Transonic and supersonic compressor test results and analyses are presented.

Publisher

ASME International

Subject

General Medicine

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Loss Reduction Using Riblets on a Supersonic Through-Flow Fan Blade Cascade;Journal of Fluids Engineering;2004-07-01

2. Supersonic Through-Flow Fan Blade Cascade Studies;Journal of Fluids Engineering;2003-09-01

3. Influence of thickness and camber on the aeroelastic stability of supersonic throughflow fans;Journal of Propulsion and Power;1991-05

4. Berechnungsunterlagen;Thermische Turbomaschinen;1966

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