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Calculation Of Heat Flux Integral Length Scales From Spatially Resolved Surface Temperature Measurements In An Engine
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Book Synopsis Calculation of Heat Flux Integral Length Scales from Spatially-Resolved Surface Temperature Measurements in an Engine by : David Boggs
Download or read book Calculation of Heat Flux Integral Length Scales from Spatially-Resolved Surface Temperature Measurements in an Engine written by David Boggs and published by . This book was released on 1991 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Spatially-resolved Measurements of Instantaneous Engine Heat Flux by : David Lee Boggs
Download or read book Spatially-resolved Measurements of Instantaneous Engine Heat Flux written by David Lee Boggs and published by . This book was released on 1990 with total page 414 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of the Influence of Integral Length Scale on Stagnation Region Heat Transfer by :
Download or read book Measurements of the Influence of Integral Length Scale on Stagnation Region Heat Transfer written by and published by . This book was released on 1994 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurement of Local High-level, Transient Surface Heat Flux by : Curt H. Liebert
Download or read book Measurement of Local High-level, Transient Surface Heat Flux written by Curt H. Liebert and published by . This book was released on 1988 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Simplified Procedures for the Calculation of Heat Transfer to Surfaces with Non-uniform Temperatures by : J. P. Hartnett
Download or read book Simplified Procedures for the Calculation of Heat Transfer to Surfaces with Non-uniform Temperatures written by J. P. Hartnett and published by . This book was released on 1956 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-speed Aircraft by : Robert D. Quinn
Download or read book A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-speed Aircraft written by Robert D. Quinn and published by . This book was released on 2000 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a method that can calculate transient aerodynamic heating and transient surface temperatures at supersonic and hypersonic speeds. This method can rapidly calculate temperature and heating rate time-histories for complete flight trajectories. Semi-empirical theories are used to calculate laminar and turbulent heat transfer coefficients and a procedure for estimating boundary-layer transition is included. Results from this method are compared with flight data from the X-15 research vehicle, YF-12 airplane, and the Space Shuttle Orbiter. These comparisons show that the calculated values are in good agreement with the measured flight data.
Book Synopsis Estimation of Highly Dynamic Heat Flux from Surface Temperature Measurements Using the Adjoint Method by : Tahar Loulou
Download or read book Estimation of Highly Dynamic Heat Flux from Surface Temperature Measurements Using the Adjoint Method written by Tahar Loulou and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Measurement of Heat Flow in the Ground and the Theory of Heat Flux Meters by : Peter Schwerdtfeger
Download or read book The Measurement of Heat Flow in the Ground and the Theory of Heat Flux Meters written by Peter Schwerdtfeger and published by . This book was released on 1970 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: The behavior of heat flux meters has been examined by experimental, electrical analogue and numerical means. The results indicate the more general applicability of the flux meter equation first proposed by Philip (1961) for the special case of spheroidal meters, provided certain precautions are taken. The purely geometric parameter appearing in this equation has been related to meter shape and a functional connection has been suggested. It is proposed that pairs of thermal sensors be used to monitor thermal conductivity continuously and the use of nonuniform 'focusing' heat flux meters is recommended in cases where the physical cross section of a thermopile should remain small compared to the resultant thermal cross section. Finally a number of calibration techniques are reported, including the use of a novel radiation enclosure in which meters are temporarily tested as net radiometers, (Author).
Book Synopsis Time-dependent Surface Temperature and Heat Flux Measurements on a Single Cylinder Engine Head and Liner by : Stephanie Treiss
Download or read book Time-dependent Surface Temperature and Heat Flux Measurements on a Single Cylinder Engine Head and Liner written by Stephanie Treiss and published by . This book was released on 2017 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Analyzing the data from both experiments, the instantaneous heat flux decayed most rapidly due to CCD at the head locations nearest the spark plug (H3 and H4). After 10 hours, the heat flux at H3 and H4 was essentially constant over the cycle, while the peak heat flux at all other locations remained at 30 to 60% of their maximum value, depending on the location. The cumulative heat flux over the cycle after 10 hours decreased to 65 to 80% of the maximum at the head locations and 90 to 100% at the liner; whereas, the head cumulative heat flux fell to 80 to 95% of their starting values and the liner to 75 to 90% after 3 hours. The deposits observed after each experiment were thicker at the head locations than the liner, with the thickest, black deposits residing at H3 and H4 where the peak heat flux declined the most. The thicknesses at H3 and H4 were 281.1 and 204.5 μm after 10 hours, and 137.6 and 138.8 μm after 3 hours, respectively. The deposit for the liner locations was thickest at L4 and L5 on the exhaust side of the engine. The deposit thicknesses at L4 and L5 were 24.0 and 24.1 μm after 10 hours, and 6.9 and 11.5 μm after 3 hours, respectively.
Book Synopsis Measurements of Integral Length Scales in an I.C. Engine by : R. A. Fraser
Download or read book Measurements of Integral Length Scales in an I.C. Engine written by R. A. Fraser and published by . This book was released on 1987 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Method for Improving Two-dimensional High Heat Flux Estimates from Surface Temperature Measurements by : D. Greg Walker
Download or read book A Method for Improving Two-dimensional High Heat Flux Estimates from Surface Temperature Measurements written by D. Greg Walker and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Diagnostics and Modeling in SI Engines by : Society of Automotive Engineers
Download or read book Diagnostics and Modeling in SI Engines written by Society of Automotive Engineers and published by SAE International. This book was released on 1996 with total page 248 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Integral Approach to Transient Heat-conduction Problems with Phase Transition by : Tse-Fou Zien
Download or read book An Integral Approach to Transient Heat-conduction Problems with Phase Transition written by Tse-Fou Zien and published by . This book was released on 1975 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate method for studying transient heat-conduction problems is presented. Its application to various linear problems and nonlinear problems involving phase transitions is described by means of several idealized problems. The method is basically a refined version of the well-known Karman-Pohlhausen integral technique in boundary-layer theory, and represents a further development of the basic ideas previously exploited to calculate skin friction and heat transfer in boundary-layer flows. The approximate solutions obtained are extensively compared with existing exact solutions and those of the classical Karman-Pohlhausen method. From the simplicity and accuracy of the present method as demonstrated in the results, the potential utility of the method in providing simple, engineering solutions to complex aerodynamic heating problems can be inferred.
Download or read book SN5001 written by E. Arbtin and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Multi-dimensional Estimation of Thermal Properties and Surface Heat Flux Using Experimental Data and a Sequential Gradient Ethod by : Kevin J. Dowding
Download or read book Multi-dimensional Estimation of Thermal Properties and Surface Heat Flux Using Experimental Data and a Sequential Gradient Ethod written by Kevin J. Dowding and published by . This book was released on 1997 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Computational Studies of Combustion and Instantaneous Heat Transfer in a Ceramic Diesel Engine by : Stefan Simescu
Download or read book Experimental and Computational Studies of Combustion and Instantaneous Heat Transfer in a Ceramic Diesel Engine written by Stefan Simescu and published by . This book was released on 1997 with total page 608 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration by : Charles B. Rumsey
Download or read book Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration written by Charles B. Rumsey and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.
