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Author : Guido Mario Baccaglini
Publisher :
ISBN 13 :
Total Pages : 226 pages
Book Rating : 4.:/5 (318 download)
Download or read book Heat Transfer to Cylinders in Flows at Low Reynolds Number written by Guido Mario Baccaglini and published by . This book was released on 1971 with total page 226 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Frederick Harold Shair
Publisher :
ISBN 13 :
Total Pages : 464 pages
Book Rating : 4.:/5 (34 download)
Download or read book Theoretical and Experimental Investigations of Fluid Flow and Heat Transfer Around a Cylinder in the Region of Low Reynolds Number and High Prandtl Number written by Frederick Harold Shair and published by . This book was released on 1963 with total page 464 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Channing Rex Robertson
Publisher :
ISBN 13 :
Total Pages : 528 pages
Book Rating : 4.F/5 ( download)
Download or read book Low Reynolds Number Shear Flow Past a Rotating Circular Cylinder written by Channing Rex Robertson and published by . This book was released on 1969 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : David Michael Rose
Publisher :
ISBN 13 :
Total Pages : 236 pages
Book Rating : 4.:/5 (34 download)
Download or read book Unsteady Heat Transfer from an Infinitely Long Circular Cylinder in a Low Reynolds Number Flow written by David Michael Rose and published by . This book was released on 1973 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : K. M. Krall
Publisher :
ISBN 13 :
Total Pages : 8 pages
Book Rating : 4.:/5 (757 download)
Download or read book ASME 70-HT/SPT-20 written by K. M. Krall and published by . This book was released on 1970 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : ROBERT L. VARWIG
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)
Download or read book Stagnation Point Heat Transfer Measurements in Hypersonic Low Reynolds Number Flows written by ROBERT L. VARWIG and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements have been made of heat transfer rates at the stagnation point of cylinders and spheres for hypersonic flow at Reynolds numbers from 5 to 500 based on nose radius. A comparison of the measurements with the predictions of Probstein and Kemp, Ferri, Zakkay and Ting, and H.K. Cheng is considered. It is concluded that, within the experimental error, ordinary boundary layer theory can be used to predict the heat transfer rates down to stagnation point Reynolds numbers of twenty. At this point, the heat transfer rate increases somewhat as predicted, reaching the free molecule value at a Reynolds number between two and three. (Author).
Author : Ivan E. Beckwith
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)
Download or read book Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers written by Ivan E. Beckwith and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design studies of hypersonic lifting vehicles have generally indicated that aerodynamic heating may be reduced by using highly swept configurations with blunted leading edges. For laminar boundary layers the effect of sweep angle A on the heat transfer at the leading edge is usually taken as cos A as shown by the data of Feller (ref. 1) who measured the average heat transfer on the front half of a swept cylinder. More recent data (refs. 2 and 3) have indicated that the effect of sweep may be more nearly cos3/2 Lambda which, at a sweep angle of 75 deg, would result in a 50-percent reduction of the heat transfer predicted by the cos A variation. The data and theory of reference 4 also indicate a cos3/2 lambda variation but the theories of references 5 and 6 indicate a variation somewhere between cos A and cos3/2 lambda for large stream Mach numbers. The data of reference 7, in contrast to the investigations just cited, showed large increases in average heat transfer to a circular leading edge with increasing A up to a lambda of about 40 deg. These increases in heat transfer were probably caused by transition to turbulent flow which apparently resulted primarily from the inherent instability of the three-dimensional boundary layer flow on a yawed cylinder. The leading-edge Reynolds numbers of reference 7 were considerably larger than the values in references 1 to 4 and were also larger than typical values for full-scale leading edges of hypersonic vehicles; hence, the main application of the high Reynolds number tests will probably be to bodies at angle of attack.
Author : Davis H. Crawford
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (31 download)
Download or read book Investigation of the Flow Over a Spiked-nose Hemisphere-cylinder at a Mach Number of 6.8 written by Davis H. Crawford and published by . This book was released on 1959 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : George A. Brown
Publisher :
ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.3/5 (91 download)
Download or read book Heat Transfer in Low Reynolds Number Flow written by George A. Brown and published by . This book was released on 1971 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Heat Transfer in low Reynolds number flow written by and published by . This book was released on 1971 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael Lenard
Publisher :
ISBN 13 :
Total Pages : 360 pages
Book Rating : 4.E/5 ( download)
Download or read book Stagnation-point Flow of a Variable-property Fluid at Low Reynolds Numbers written by Michael Lenard and published by . This book was released on 1962 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt: Steady, viscous, two-dimensional and axially symmetric stagnation-point flows of a gas are considered for the case when the Reynolds number is too low for the applicability of the classical boundary-layer theory. It is assumed that the low-density gas is still a continuous fluid, permitting the use of the Navier-Stokes and as associated equations as the basis of the problem. The effects of low Reynolds number are determined by applying an expansion procedure to the fluid dynamical equations.
Author : Paige B. Burbank
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)
Download or read book Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 written by Paige B. Burbank and published by . This book was released on 1959 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.:/5 (227 download)
Download or read book FORCED CONVECTIVE HEAT TRANSFER TO COOLED CYLINDERS AT LOW REYNOLDS NUMBERS AND WITH LARGE TEMPERATURE DIFFERENCES. written by and published by . This book was released on 1968 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: For the purpose of determining a general correlation for forced convective heat transfer coefficients for circular cylinders in cross-flow under conditions pertaining to cooled-film application for measurements in flames and hypersonic wakes, heat transfer measurements were obtained under simulated conditions created in a plasma-jet. Measurements were made by means of constant temperature, internally cooled, cylindrical film sensors in the Reynolds number range 5-75 for various temperature loadings, the maximum being T sub infinity/T sub s = 4, and for flows composed of He, N2 and CO2. The plasma-jet conditions were maintained such that at the points of measurements, i.e. at the potential core of the jet, ionization was negligible, recombination was complete and the turbulence intensity was low. All the fluid property values in the dimensionless parameters were evaluated at the arithmetic mean temperature. A kinematic viscosity ratio instead of the more usual temperature ratio was considered in the temperature loading factor to account for the different dependency of the transport properties on temperature for different gas species. (Author).
Author : Stanford University. Department of Mechanical Engineering
Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.F/5 ( download)
Download or read book Heat Transfer from Rotating Bodies: Part I, the Horizontal Cylinder in an Infinite Environment written by Stanford University. Department of Mechanical Engineering and published by . This book was released on 1955 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Victor Manuel Feliz Pérez
Publisher :
ISBN 13 :
Total Pages : 296 pages
Book Rating : 4.E/5 ( download)
Download or read book The Effect of Heat Transfer on Low Reynolds Number Downward Flow of Newtonian Fluids in a Vertical Pipe written by Victor Manuel Feliz Pérez and published by . This book was released on 1973 with total page 296 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Kenneth Mark Krall
Publisher :
ISBN 13 :
Total Pages : 452 pages
Book Rating : 4.:/5 (319 download)
Download or read book Local Heat Transfer Around a Transverse Circular Cylinder in Slip Flow written by Kenneth Mark Krall and published by . This book was released on 1969 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : A. Zhukauskas
Publisher : Core/Mechanical
ISBN 13 :
Total Pages : 232 pages
Book Rating : 4.3/5 (91 download)
Download or read book Heat Transfer of a Cylinder in Crossflow written by A. Zhukauskas and published by Core/Mechanical. This book was released on 1985 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt:
