Author: Donald A. Petrash
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 38
Book Description
Design and Experimental Investigation of a High-weight-flow Low-pressure-ratio Turbine
Author: Donald A. Petrash
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 38
Book Description
Design and Experimental Investigation of Two Rotor Blade Modifications for a High-weight-flow Low-pressure-ratio Turbine
Author: Robert R. Nunamaker
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 32
Book Description
Design and Experimental Investigation of a Single-stage Turbine with a Rotor Entering Relative Mach Number of 2
Author: Thomas P. Moffitt
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 34
Book Description
Experimental Investigation of Partial- and Full-admission Characteristics of a Two-stage Velocity-compounded Turbine
Author: Thomas P. Moffitt
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 26
Book Description
An Experimental Investigation of a Subscale Variable Pressure Ratio High Thru Flow Turbine
Author: D. J. Helton
Publisher:
ISBN:
Category :
Languages : en
Pages : 91
Book Description
This program investigates the aerodynamics of a subscale model of a variable pressure ratio high through flow turbine. The problem areas are: Small limit loading margin, High rotor relative inlet Mach number, Low aspect ratio blading, Large rotor turning, and Low hub/tip radius ratio.
Publisher:
ISBN:
Category :
Languages : en
Pages : 91
Book Description
This program investigates the aerodynamics of a subscale model of a variable pressure ratio high through flow turbine. The problem areas are: Small limit loading margin, High rotor relative inlet Mach number, Low aspect ratio blading, Large rotor turning, and Low hub/tip radius ratio.
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 428
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 428
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 748
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 748
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Experimental Investigation of Boundary Layer Behavior in a Simulated Low Pressure Turbine
Author: Ki-Hyeon Sohn
Publisher:
ISBN:
Category : Boundary layers
Languages : en
Pages : 16
Book Description
Publisher:
ISBN:
Category : Boundary layers
Languages : en
Pages : 16
Book Description
Experimental Investigation of Partial and Full-admission Characteristics of a Two- Stage Velocity-compound Turbine
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Experimental Investigation of a 4 and 1/2 Stage Turbine with Very High Stage Loading Factor. 2: Turbine Performance
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 102
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 102
Book Description