Author: Richard P. GeyePublisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Investigation of Effects of Reynolds Number on Over-all Performance of an Eight-stage Axial-flow Research Compressor with Two Transonic Inlet Stages
Author: Richard P. GeyeInvestigation of Reynolds Number Effect on Performance of an Eight-stage Axial-flow Research Compressor with Long- and Medium-chord Lengths in the Two Transonic Inlet Stages
Author: Gilbert K. SieversPublisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 21
Book Description
The chords of the first two stages of an eight-stage axial-flow compressor with two transonic inlet stages were doubled, and the effects of Reynolds number on the over-all performance were investigated and compared with those of the original compressor.
Investigation of the Effects of Low Reynolds Number Operation on the Performance of a Single-Stage Turbine with a Downstream Stator
Author: Robert E. ForrettePublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52
Book Description
Aerothermodynamics of Aircraft Engine Components
Author: Gordon C. OatesPublisher: AIAA
ISBN: 9781600860058
Category : Aerothermodynamics
Languages : en
Pages : 568
Book Description
Annotation Design and R & D engineers and students will value the comprehensive, meticulous coverage in this volume. Beginning with the basic principles and concepts of aeropropulsion combustion, chapters explore specific processes, limitations, and analytical methods as they bear on component design.
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
The Aerothermodynamics of Aircraft Gas Turbine Engines
Author: Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Investigation of a High-pressure-ratio Eight-stage Axial-flow Research Compressor with Two Transonic Inlet Stages
Author: Richard P. GeyeIndex to NASA Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Author: