Author: Louis M. Russell
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 20
Book Description
Flow Visualization of Discrete-hole Film Cooling with a Spawnwise Injection Over a Cylinder
Author: Louis M. Russell
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 20
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1088
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1088
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1094
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1094
Book Description
Streakline flow visualization of discrete-hole film cooling with normal, slanted and compound angle injection
Author: Raymond S. Colladay
Publisher:
ISBN:
Category : Flow visualization
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Flow visualization
Languages : en
Pages : 28
Book Description
Streakline flow visualization of discrete hole film cooling with holes inclined 30 ĚŠto surface
Author: Raymond S. Colladay
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 22
Book Description
Stagnation Region Gas Film Cooling
Author: D. W. Luckey
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 388
Book Description
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 388
Book Description
Effect on Gaseous Film Cooling of Coolant Injection Through Angled Slots and Normal Holes
Author: S. Stephen Papell
Publisher:
ISBN:
Category : Cooling
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Cooling
Languages : en
Pages : 32
Book Description
Full-coverage Film Cooling on Flat, Isothermal Surfaces
Author: Michael E. Crawford
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 120
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 120
Book Description
Vortex-Generating Coolant-Flow-Passage Design for Increased Film-Cooling Effectiveness and Surface Coverage
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724765208
Category :
Languages : en
Pages : 28
Book Description
The thermal film-cooling footprints observed by infrared imagery for three coolant-passage configurations embedded in adiabatic-test plates are discussed. The configurations included a standard round-hole cross section and two orientations of a vortex-generating flow passage. Both orientations showed up to factors of four increases in both film-cooling effectiveness and surface coverage over that obtained with the round coolant passage. The crossflow data covered a range of tunnel velocities from 15.5 to 45 m/sec with blowing rates from 0.20 to 2.05. A photographic streakline flow visualization technique supported the concept of the counterrotating apability of the flow passage design and gave visual credence to its role in inhibiting flow separation. Papell, S. S. Glenn Research Center NASA-TP-2388, E-2147, NAS 1.60:2388 RTOP 505-41-32
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724765208
Category :
Languages : en
Pages : 28
Book Description
The thermal film-cooling footprints observed by infrared imagery for three coolant-passage configurations embedded in adiabatic-test plates are discussed. The configurations included a standard round-hole cross section and two orientations of a vortex-generating flow passage. Both orientations showed up to factors of four increases in both film-cooling effectiveness and surface coverage over that obtained with the round coolant passage. The crossflow data covered a range of tunnel velocities from 15.5 to 45 m/sec with blowing rates from 0.20 to 2.05. A photographic streakline flow visualization technique supported the concept of the counterrotating apability of the flow passage design and gave visual credence to its role in inhibiting flow separation. Papell, S. S. Glenn Research Center NASA-TP-2388, E-2147, NAS 1.60:2388 RTOP 505-41-32