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Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading / Kerry L. McLallin, Jeffrey E. Hass.

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Format:
Book
Government document
Author/Creator:
McLallin, Kerry L., author.
Haas, Jeffrey E., author.
Contributor:
Lewis Research Center
Propulsion Laboratory (U.S.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Series:
NASA technical paper ; 1730.
AVRADCOM technical report ; 80-09.
NASA technical paper ; 1730
AVRADCOM technical report ; 80-09
Language:
English
Subjects (All):
Aircraft gas-turbines--Blades.
Aircraft gas-turbines.
Aerodynamic load.
Turbines--Aerodynamics.
Turbines.
Genre:
Online resources.
Physical Description:
1 online resource (18 pages) : illustrations
Place of Publication:
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1980.
Notes:
Title from title screen (viewed on August 16, 2016).
"October 1980."
"Performing Organization: NASA Lewis Research Center and Propulsion Laboratory, AVRADCOM Research and Technology Laboratories"--Report documentation page
Includes bibliographical references (pages 17-18).
Other Format:
Print version: McLallin, Kerry L. Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
Microfiche version: McLallin, Kerry L. Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
OCLC:
762118239

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