Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Transpiration Cooling Of A Cylinder In Cross Flow With Helium Injection
Download Transpiration Cooling Of A Cylinder In Cross Flow With Helium Injection full books in PDF, epub, and Kindle. Read online Transpiration Cooling Of A Cylinder In Cross Flow With Helium Injection ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Transpiration Cooling of a Cylinder in Cross Flow with Helium Injection by : Lawrence Steve Jurewicz
Download or read book Transpiration Cooling of a Cylinder in Cross Flow with Helium Injection written by Lawrence Steve Jurewicz and published by . This book was released on 1961 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transpiration Cooling of a Cylinder in Crossflow by : E. Elzy
Download or read book Transpiration Cooling of a Cylinder in Crossflow written by E. Elzy and published by . This book was released on 1967 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transpiration Cooling of a Cylinder in Crossflow; an Experimental Investigation by : Amrik Singh Ahluwalta
Download or read book Transpiration Cooling of a Cylinder in Crossflow; an Experimental Investigation written by Amrik Singh Ahluwalta and published by . This book was released on 1971 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transpiration Cooling Experiments Near the Stagnation Line of a Cylinder in Cross Flow by : Richard L. Humphrey
Download or read book Transpiration Cooling Experiments Near the Stagnation Line of a Cylinder in Cross Flow written by Richard L. Humphrey and published by . This book was released on 1970 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were made with a cylindrical model transpiration cooled over a region plus or minus 15 deg. from the stagnation line. Air was used as the coolant. The model was tested at a nominal Mach number of 7.0. Wall temperatures and heat-transfer rates were in good agreement with predicted values. The effect of the external pressure distribution on the local coolant flow rate and wall temperature is discussed. (Author).
Book Synopsis Exploratory Investigation of Transpiration Cooling of a 40° Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures of 1,295° to 2,910° F by : Bernard Rashis
Download or read book Exploratory Investigation of Transpiration Cooling of a 40° Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures of 1,295° to 2,910° F written by Bernard Rashis and published by . This book was released on 1957 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: The results presented herein were obtained in a transpiration cooling investigation of a double wedge of 40° included angle having a porous stainless-steel specimen inserted flush with the top surface of the wedge. Nitrogen and helium were used as coolants, and tests were conducted for stagnation temperatures ranging from 1,295° to 2,910° F. The data for both the nitrogen and helium coolants indicated greater cooling effectiveness than predicted by theory and were in good agreement with the results for an 8° cone tested at a stagnation temperature of 600° F.
Book Synopsis Transpiration Cooling Experiments Near the Stagnation Line of a Cylinder in Cross Flow by : Richard L. Humphrey
Download or read book Transpiration Cooling Experiments Near the Stagnation Line of a Cylinder in Cross Flow written by Richard L. Humphrey and published by . This book was released on 1970 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were made with a cylindrical model transpiration cooled over a region plus or minus 15 deg. from the stagnation line. Air was used as the coolant. The model was tested at a nominal Mach number of 7.0. Wall temperatures and heat-transfer rates were in good agreement with predicted values. The effect of the external pressure distribution on the local coolant flow rate and wall temperature is discussed. (Author).
Book Synopsis Exploratory Investigation of Transpiration Cooling of a 40 Degree Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures from 1,295 Degrees F to 2,910 Degrees F by : Bernard Rashis
Download or read book Exploratory Investigation of Transpiration Cooling of a 40 Degree Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures from 1,295 Degrees F to 2,910 Degrees F written by Bernard Rashis and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Analytical and Experimental Investigation of a Transpiration Cooled Cylinder Subjected to a Cross Flow by : Joseph Rudolph Cherney
Download or read book An Analytical and Experimental Investigation of a Transpiration Cooled Cylinder Subjected to a Cross Flow written by Joseph Rudolph Cherney and published by . This book was released on 1968 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Exploratory Investigation of Transpiration Cooling of a 40 Degree Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures from 1,295 Degrees F to 2,910 Degrees F by : Bernard Rashis
Download or read book Exploratory Investigation of Transpiration Cooling of a 40 Degree Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures from 1,295 Degrees F to 2,910 Degrees F written by Bernard Rashis and published by . This book was released on 1961 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of transpiration cooling was conducted in the preflight jet of the Langley Pilotless Aircraft Research Station at Wallops Island, Va. The model consisted of a double wedge of 40 degrees included angle having a porous stainless-steel specimen inserted flush with the top surface of the wedge. The tests were conducted at a free-stream Mach number of 2.0 for stagnation temperatures ranging from 1,295 F to 2,910 F. Nitrogen and helium were used as coolants and tests were conducted for values ranging from approximately 0.03 to 0.30 percent of the local weight flow rate. The data for both the nitrogen and helium coolants indicated greater cooling effectiveness than that predicted by theory and were in good agreement with the results for an 8 degree cone tested at a stagnation temperature of 600 F. The results indicate that the helium coolant, for the same amount of heat-transfer reduction, requires only about one-fourth to one-fifth the coolant flow weight as the nitrogen coolant. (Author).
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Film Cooling with Air and Helium Injection Through a Rearward-facing Slot Into a Superonic Air Flow by : R. J. Goldstein
Download or read book Film Cooling with Air and Helium Injection Through a Rearward-facing Slot Into a Superonic Air Flow written by R. J. Goldstein and published by . This book was released on 1965 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Exploratory Tests of Transpiration Cooling on a Porous 8 Degree Cone at M by : Leo T. Chauvin
Download or read book Exploratory Tests of Transpiration Cooling on a Porous 8 Degree Cone at M written by Leo T. Chauvin and published by . This book was released on 1955 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effectiveness of transpiration cooling on an 8 degree total-angle conical body having a porous skin is presented for various coolant mass flow rates of nitrogen gas, helium gas, and distilled water. The tests were made under steady flow conditions in a free jet at a Mach number 0f 2.05, and at a Reynolds number of 8,000,000 based on approximately sea-level conditions and on the length of porous section investigated. Good agreement for the nitrogen tests was obtained with a theory for transpiration cooling. Helium gas gave the same reduction in heat transfer for less flow rate than the nitrogen gas. Tests with distilled water gave a large reduction in the average skin temperature. In the transpiration tests of this report, the model was completely cooled for a rate of 3.57 lb/min-ft sq; whereas for the film-cooling tests cooling the same model required 3.78 lb/min-ft sq.
Book Synopsis Progress in Heat and Mass Transfer by :
Download or read book Progress in Heat and Mass Transfer written by and published by . This book was released on 1971 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Journal of Heat Transfer written by and published by . This book was released on 1964 with total page 1216 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Mechanical Engineering written by and published by . This book was released on 1968 with total page 1130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Handbook of Heat Transfer Applications by : Warren M. Rohsenow
Download or read book Handbook of Heat Transfer Applications written by Warren M. Rohsenow and published by McGraw-Hill Companies. This book was released on 1985 with total page 986 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Mechanical & Chemical Engineering Transactions by :
Download or read book Mechanical & Chemical Engineering Transactions written by and published by . This book was released on 1965 with total page 686 pages. Available in PDF, EPUB and Kindle. Book excerpt: