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Experimental Investigation Of The Heat Transfer Characteristics Of An Air Cooled Sintered Porous Turbine Blade
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Book Synopsis Experimental Investigation of the Heat-transfer Characteristics of an Air-cooled Sintered Porous Turbine Blade by : Louis J. Schafer (Jr.)
Download or read book Experimental Investigation of the Heat-transfer Characteristics of an Air-cooled Sintered Porous Turbine Blade written by Louis J. Schafer (Jr.) and published by . This book was released on 1952 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Analytical Investigation of Heat-transfer Characteristics of a Return-flow Air-cooled Turbine Rotor Blade by : Francis S. Stepka
Download or read book Experimental and Analytical Investigation of Heat-transfer Characteristics of a Return-flow Air-cooled Turbine Rotor Blade written by Francis S. Stepka and published by . This book was released on 1959 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Cooling Characteristics of Transpiration Air-cooled Turbine Blades in a High Temperature Gas Cascade by : Ronald Lang
Download or read book Experimental Investigation of the Cooling Characteristics of Transpiration Air-cooled Turbine Blades in a High Temperature Gas Cascade written by Ronald Lang and published by . This book was released on 1958 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted on a transpiration air cooled stator cascade to evaluate the heat transfer characteristics, to observe the temperature patterns, and to verify the existing transpiration cooling theory for hot gas streams ranging in temperature from 1600 to 2050 F.A total of 49 hours and 55 minutes of cascade testing were logged. Hot gas Reynolds numbers computed at ten span-wise positions on the blade varied between 7800 on the pressure side near the leading edge and 288,000 at the convex side just upstream of the trailing edge. Hot gas weight flows of 2.46 lb/sec and 1.64 lb/sec were directed at the cascade section. A comprehensive analysis of the data accumulated along with detailed descriptions of the test facility, the component test hardware, and the problems associated with instrumentation is presented.
Book Synopsis Analytical and Experimental Investigation of a Forced-convection Air-cooled Internal Strut-supported Turbine Blade by : Eugene F. Schum
Download or read book Analytical and Experimental Investigation of a Forced-convection Air-cooled Internal Strut-supported Turbine Blade written by Eugene F. Schum and published by . This book was released on 1954 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine by : Robert O. Hickel
Download or read book Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine written by Robert O. Hickel and published by . This book was released on 1950 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Coolant-flow Characteristics of a Sintered Porous Turbine Blade by : Edward R. Bartoo
Download or read book Experimental Investigation of Coolant-flow Characteristics of a Sintered Porous Turbine Blade written by Edward R. Bartoo and published by . This book was released on 1952 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine by : Jack B. Esgar
Download or read book Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine written by Jack B. Esgar and published by . This book was released on 1952 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Survey of Advantages and Problems Associated with Transpiration Cooling and Film Cooling of Gas-turbine Blades by : Ernst Rudolf Georg Eckert
Download or read book Survey of Advantages and Problems Associated with Transpiration Cooling and Film Cooling of Gas-turbine Blades written by Ernst Rudolf Georg Eckert and published by . This book was released on 1951 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Transpiration and film cooling promise to be effective methods of cooling gas-turbine blades; consequently, analytical and experimental investigations are being conducted to obtain a better understanding of these processes. This report serves as an introduction to these cooling methods, explains the physical processes, and surveys the information available for predicting blade temperatures and heat-transfer rates. In addition, the difficulties encountered in obtaining a uniform blade temperature are discussed, and the possibilities of correcting these difficulties are indicated. Air is the only coolant considered in the application of these cooling methods.
Book Synopsis Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine by : Vernon L. Arne
Download or read book Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine written by Vernon L. Arne and published by . This book was released on 1951 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine by : Herman H. Ellerbrock (Jr.)
Download or read book Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine written by Herman H. Ellerbrock (Jr.) and published by . This book was released on 1951 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Study of the Heat Transfer Characteristics of a Turbine Blade Having a Ceramic Sleeve with Air Cooling by : David Eugene Dressendorfer
Download or read book A Study of the Heat Transfer Characteristics of a Turbine Blade Having a Ceramic Sleeve with Air Cooling written by David Eugene Dressendorfer and published by . This book was released on 1949 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1959 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 750 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NACA Research Memorandum written by and published by . This book was released on 1955 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Research Abstracts and Reclassification Notice by : United States. National Advisory Committee for Aeronautics
Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 596 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Memorandum written by and published by . This book was released on 1958 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Chord Size on Weight and Cooling Characteristics of Air-cooled Turbine Blades by : Jack B. Esgar
Download or read book Effect of Chord Size on Weight and Cooling Characteristics of Air-cooled Turbine Blades written by Jack B. Esgar and published by . This book was released on 1957 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis has been made to determine the effect of chord size on the weight and cooling characteristics of shell-supported, air-cooled gas-turbine blades. In uncooled turbines with solid blades, the general practice has been to design turbines with high aspect ratio (small blade chord) to achieve substantial turbine weight reduction. With air-cooled blades, this study shows that turbine blade weight is affected to a much smaller degree by the size of the blade chord.
