Author: Donald A. PetrashPublisher:
ISBN:
Category : Air flow
Languages : en
Pages : 26
Book Description
Component Performance Investigation of J71 Experimental Turbine
Author: Donald A. PetrashPublisher:
ISBN:
Category : Air flow
Languages : en
Pages : 26
Book Description
COMPONENT PERFORMANCE INVESTIGATION OF J71 EXPERIMENTAL TURBINE. 4. EFFECT OF FIRST-STATOR ADJUSTMENT ; OVER-ALL PERFORMANCE OF J71-97 TURBINE WITH 132-PERCENT-DESIGN STATOR AREA.
Author: Component Performance Investigation of L71 Experimental Turbine
Author: Donald A. PetrashPublisher:
ISBN:
Category : Air flow
Languages : en
Pages : 19
Book Description
The changes in the internal flow conditions resulting from adjusting the first-stator throat area of the J71 experimental three-stage turbine were investigated. Presented herein are the experimental results of interstage flow measurements obtained from a radial survey investigation conducted on this turbine when equipped with a first-stage stator with a throat area increased to 132 percent of the design area and operated at a single predetermined turbine match point. Radial variations and mass-averaged values of stage efficiency were determined, along with Mach number and flow angle distributions behind each blade row.
Experimental Investigation of Stage Performance of J71 Three-stage Turbine
Author: Robert E. ForretteComparison of Results of Experimental and Theoretical Studies of Blade-outlet Boundary-layer Characteristics of Stator Blade for a High Subsonic Mach Number Turbine
Author: Cavour H. HauserPublisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 30
Book Description
Experimental Investigation of Two-stage Air-cooled Turbine Suitable for Flight at Mach 2.5
Author: Harold J. SchumPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 54
Book Description
NASA Technical Note
Author: Turbine Aerodynamic and Cooling Requirements for a Turbojet Powered Mach 3 Transport Using Methane Fuel
Author: David G. EvansPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 92
Book Description
Experimental Investigation of Two-stage Air-cooled Turbine Suitable for Flight at Mach 2.5
Author: Performance Improvement Through Indexing of Turbine Airfoils - Part 1 - Experimental Investigation
Author: F. W. HuberPublisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine and Aeroengine Congress & Exposition, Houston, Texas - June 5-8, 1995.