Accession Number:

ADA182996

Title:

Transonic and Supersonic Phenomena in Turbomachines: Proceedings of the Propulsion and Energetics (68th)(B) Specialists' Meeting Held in Munich, Germany on 10-12 September 1986

Descriptive Note:

Conference proceedings

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1987-03-01

Pagination or Media Count:

357.0

Abstract:

Contents Shock Structure Measured In A Transonic Fan Using Laser Anemometry, Wake and Shock Interactions In A Transonic Turbine Stage, The Boundary Layer Behaviour of Highly Loaded Compressor Cascade At Transonic Flow Conditions, Vortex Shedding In Compressor Blade Wakes, Experimental Observations On An Unsteady, Normal ShockBoundary Layer Interaction, Measured And Predicted Loss Generation In Transonic Turbine Blading, Influence Of Shock And Boundary Losses On The Performance Of Highly Loaded Supersonic Axial Flow Compressors, Experimental Investigations On Shock Losses Of Transonic And Supersonic Compressor Cascades, Optimization Of A Transonic Flow Radial Vaned Diffuser, A Quasi Three Dimensional Method For The Calculation Of Transonic Flow In Turbomachines, Transonic Three Dimensional Inviscid Calculations In Turbomachines, Computation Of Transonic 2D-Cascade Flow And Comparison With Experiments, A Numerical Study Of Unsteady Flow Effects In A Supersonic Compressor Cascade, A Numerical Study Of The 3D Flowfield In A Transonic Compressor Rotor With A Modelling Of the Tip Clearance Flow, Some Turbomachinery Blade Passage Analysis Methods-Retrospect And Prospect, Downstream Flow Angle Correlations For Turbine Cascades In Subsonic And Transonic Flow Conditions, Comparison Between Inverse Design PVD Airfoils And Standard Series Airfoils For High Loaded Axial Turbine Nozzle Application.

Subject Categories:

  • Hydraulic and Pneumatic Equipment
  • Fluid Mechanics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE