Author: A. Richard FelixPublisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 50
Book Description
A Comparison of Typical National Gas Turbine Establishment and NACA Axial-flow Compressor Blade Sections in Cascade at Low Speed
Author: A. Richard FelixPublisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 50
Book Description
A Comparison of Typical National Gas Turbine Establishment and NACA Axial-flow Compressor Blade Sections in Cascade at Low Speed
Author: A. Richard FelixPublisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 46
Book Description
Comparative cascade tests of the NGTE (National Gas Turbine Establishment of Great Britain) 10C4/30C50 and NACA 65-(12A10)10 axial flow compressor blade sections were conducted in a 5-inch low-speed cascade tunnel at the Langley Laboratory at air-inlet angles of 30 degrees, 45 degrees, and 60 degrees and a solidity of 1.0 by using the porous-wall technique. These NACA data for the NGTE 10C4/30C50 section were also compared with data from NGTE design charts for the same section. British and NACA incompressible cascade force-analysis equations are included.
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 306
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
Book Description
Annual Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 530
Book Description
U.S. Government Research Reports
Author: Publisher:
ISBN:
Category : Science
Languages : en
Pages : 56
Book Description
Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508
Book Description
Experimental Study of Heat Transfer to Small Cylinders in a Subsonic, High-temperature Gas Stream
Author: George E. GlawePublisher:
ISBN:
Category : Combustion gases
Languages : en
Pages : 820
Book Description
A Nusselt-Reynolds number relation for cylindrical thermocouple wires in crossflow was obtained from the experimental determination of time constants. Tests were conducted in exhaust gas over a temperature range of 2000 to 3400 R, a Mach number range of 0.3 to 0.8, and a static-pressure range from 2/3 to 1-1/3 atmospheres, yielding a Reynolds number range of 450 to 3000. The correlation obtained is Nu=(0.428 plus or minus 0.003) times the square root of Re with average deviations of a single observation of 8.5 percent. This relation is the same as one previously reported for room-temperature conditions.
Applied Mechanics Reviews
Author: Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 630
Book Description
