National Technical Reports Library

The National Technical Information Service acquires, indexes, abstracts, and archives the largest collection of U.S. government-sponsored technical reports in existence. The NTRL offers online, free and open access to these authenticated government technical reports. Technical reports and documents in its repository may be available online for free either from the issuing federal agency, the U.S. Government Publishing Office’s Federal Digital System website, or through search engines.

Details

ADA304883

Publication Date	1996
Page Count	582
Abstract	No abstract available.
Keywords	Computational fluid dynamics Unsteady flow Gas turbines Cascades(Fluid dynamics) Heat transfer Pressure gradients Mathematical models Computerized simulation Nato Shock waves Leakage(Fluid) Turbulent boundary layer Vortices Flow visualization Pressure measurement Mass flow Flow fields Stalling Wake Losses Boundary layer transition Gas turbine blades Navier stokes equations Inviscid flow Viscous flow Flow separation Pressure distribution Dynamic pressure Gas surface interactions Aerodynamics Transonic flow Steady flow Three dimensional flow Turbojet engines Compressor stators Secondary flow Axial flow compressors Blade tips Rotor blades(Turbomachinery) Engine surge Turbine stators Foreign technology Nato furnished
Source Agency	Non Paid ADAS
NTIS Subject Category	46B - Fluid Mechanics 81D - Jet & Gas Turbine Engines 51A - Aerodynamics
Corporate Authors	Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine (France).
Supplemental Notes	Papers Presented at the Propulsion and Energetic Panel (PEP) 85th Symposium, Derby, UK 8-12 May 95. Preface in French and English.
Document Type	Technical Report
NTIS Issue Number	199616

Loss Mechanisms and Unsteady Flows in Turbomachines (Les Mechanismes des Pertes et Les Ecoulements Instationnaires dans Les Turbomachines).

Loss Mechanisms and Unsteady Flows in Turbomachines (Les Mechanismes des Pertes et Les Ecoulements Instationnaires dans Les Turbomachines).
ADA304883

Publication Date	1996
Page Count	582
Abstract	No abstract available.
Keywords	Computational fluid dynamics Unsteady flow Gas turbines Cascades(Fluid dynamics) Heat transfer Pressure gradients Mathematical models Computerized simulation Nato Shock waves Leakage(Fluid) Turbulent boundary layer Vortices Flow visualization Pressure measurement Mass flow Flow fields Stalling Wake Losses Boundary layer transition Gas turbine blades Navier stokes equations Inviscid flow Viscous flow Flow separation Pressure distribution Dynamic pressure Gas surface interactions Aerodynamics Transonic flow Steady flow Three dimensional flow Turbojet engines Compressor stators Secondary flow Axial flow compressors Blade tips Rotor blades(Turbomachinery) Engine surge Turbine stators Foreign technology Nato furnished
Source Agency	Non Paid ADAS
NTIS Subject Category	46B - Fluid Mechanics 81D - Jet & Gas Turbine Engines 51A - Aerodynamics
Corporate Authors	Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine (France).
Supplemental Notes	Papers Presented at the Propulsion and Energetic Panel (PEP) 85th Symposium, Derby, UK 8-12 May 95. Preface in French and English.
Document Type	Technical Report
NTIS Issue Number	199616