Author: Louis J. GoldmanPublisher:
ISBN:
Category : Blades
Languages : en
Pages : 50
Book Description
Laser Anemometer Measurements in an Annular Cascade of Core Turbine Vanes and Comparison with Theory
Author: Louis J. GoldmanPublisher:
ISBN:
Category : Blades
Languages : en
Pages : 50
Book Description
Laser Anemometer Measurements and Computations in an Annular Cascade of High Turning Core Turbine Vanes
Author: Louis J. GoldmanPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Laser Anemometer Measurements and Computations for Transonic Flow Conditions in an Annular Cascade of High Turning Core Turbine Vanes
Author: Louis J. GoldmanPublisher:
ISBN:
Category : Laser Doppler velocimeter
Languages : en
Pages : 40
Book Description
Three Component Laser Anemometer Measurements in an Annular Cascade of Core Turbine Vanes with Contoured End Wall
Author: Louis J. GoldmanPublisher:
ISBN:
Category : Laser Doppler velocimeter
Languages : en
Pages : 48
Book Description
NASA Technical Paper
Author: NASA Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 418
Book Description
Laser Anemometer Measurements and Computations in an Annular Cascade of High Turning Core Turbine Vanes
Author: Louis J. GoldmanGeneration of a Composite Grid for Turbine Flows and Consideration of a Numerical Scheme
Author: Y. ChooPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26
Book Description
A composite grid was generated for flows in turbines. It consisted of the C-grid (or O-grid) in the immediate vicinity of the blade and the H-grid in the middle of the blade passage between the C-grids and in the upstream region. This new composite grid provides better smoothness, resolution, orthogonality than any single grid for a typical turbine blade with a large camber and rounded leading and trailing edges. The C-H (or O-H) composite grid has an unusual grid point that is connected to more than four neighboring nodes in two dimensions (more than six neighboring nodes in three dimensions). A finite-volume lower-upper (LU) implicit scheme to be used on this poses no problem and requires no special treatment because each interior cell of this composite grid has only four neighboring cells in two dimensions (six cells in three dimensions). The LU implicit scheme was demonstrated to be efficient and robust for external flows in a broad flow regime and can be easily applied to internal flows and extended from two to three dimensions.
Three-component Laser Anemometer Measurement Systems
Author: Louis J. GoldmanPublisher:
ISBN:
Category : Fluid dynamic measurements
Languages : en
Pages : 24
Book Description
Laser Anemometer Measurements in a Transonic Axial-flow Fan Rotor
Author: Anthony J. StrazisarPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 220
Book Description