Efficiency and Drag of an Axial-Flow Compressor Stage: The Connexion Between the Efficiency of a Stage, the Forces on the Blade Sections and the Profile Drag; the Relation Between Different Definitions of Efficiency, and the Effect of other Sources of Loss

By Stephenson J.M.  

Aircraft Engineering, Vol. 25, Iss. 6, 1993-12 ,pp. : 158-160

Emerald Group Publishing Ltd

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A Comparison of Axial and Centrifugal Compressor Gas Turbines: An Objective Examination of the Pros and Cons of a Much Debated Subject

By F.R.Ae.S. A.D. Baxter   M.Eng.   M.I.Mech.E.  

Aircraft Engineering, Vol. 24, Iss. 7, 1993-12 ,pp. : 186-197

Emerald Group Publishing Ltd

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A model governing the stall characteristics of an isolated axial compressor rotor

By Canbazoglu Suat   Yilbas Bekir Sami  

Aircraft Engineering, Vol. 77, Iss. 2, 2005-04 ,pp. : 142-147

Emerald Group Publishing Ltd

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Propeller Development

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Aircraft Engineering, Vol. 53, Iss. 8, 1993-12 ,pp. : 16-18

Emerald Group Publishing Ltd

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Inlet Flow Field Simulation Techniques for Engine/Compressor Testing

By Younghans J.L.   Moore M.T.   Collins T.P.   Direnzi J.G.  

Aircraft Engineering, Vol. 42, Iss. 11, 1993-12 ,pp. : 12-17

Emerald Group Publishing Ltd

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