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Experimental And Analytical Sonic Nozzle Discharge Coefficients For Reynolds Numbers Up To 8x106
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Book Synopsis Experimental and Analytical Sonic Nozzle Discharge Coefficients for Reynolds Numbers Up to 8x106 by : Andrew J. Szaniszlo
Download or read book Experimental and Analytical Sonic Nozzle Discharge Coefficients for Reynolds Numbers Up to 8x106 written by Andrew J. Szaniszlo and published by . This book was released on 1975 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Analytical Sonic Nozzle Discharge Coefficients for Reynolds Numbers Up to 8 X 10 to the 6th Power by : A. J. Szaniszlo
Download or read book Experimental and Analytical Sonic Nozzle Discharge Coefficients for Reynolds Numbers Up to 8 X 10 to the 6th Power written by A. J. Szaniszlo and published by . This book was released on 1975 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Analytical Sonic Nozzle Discharge Coefficients for Reynolds Number Up to 8x10(to the Power of 6) by : Andrew J. Szaniszlo
Download or read book Experimental and Analytical Sonic Nozzle Discharge Coefficients for Reynolds Number Up to 8x10(to the Power of 6) written by Andrew J. Szaniszlo and published by . This book was released on 1975 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1974 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analytic Determination of the Discharge Coefficients of Flow Nozzles by : Frederick S. Simmons
Download or read book Analytic Determination of the Discharge Coefficients of Flow Nozzles written by Frederick S. Simmons and published by . This book was released on 1955 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: Integration of the velocity profile at the throat of a flow nozzle yields the discharge coefficient as a function of the ratio of boundary-layer thickness to the nozzle diameter. This ratio is obtained as a solution of the approximate momentum equation for the boundary layer. The resulting expression for the discharge coefficient is then a function of the Reynolds number based on nozzle diameter and of the geometry of the nozzle. Good agreement is shown between this expression and published experimental data on flow nozzles for Reynolds numbers between 10,000 and 1,000,000.
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1961 with total page 1096 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Paper written by and published by . This book was released on 1974 with total page 314 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Journal of Engineering for Power by :
Download or read book Journal of Engineering for Power written by and published by . This book was released on 1974 with total page 1160 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 1975 with total page 790 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cumulative Index to Transactions of the ASME. by :
Download or read book Cumulative Index to Transactions of the ASME. written by and published by . This book was released on 1976 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt: Indexes the journals which continue American Society of Mechanical Engineers. Transactions. and which are also called: Series A- of the Transactions of the American Society of Mechanical Engineers.
Book Synopsis Evaluation of Reynolds Number and Tunnel Wall Porosity Effects on Nozzle Afterbody Drag at Transonic Mach Numbers by : C. E. Robinson
Download or read book Evaluation of Reynolds Number and Tunnel Wall Porosity Effects on Nozzle Afterbody Drag at Transonic Mach Numbers written by C. E. Robinson and published by . This book was released on 1976 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to study the effects of Reynolds number variation on isolated nozzle afterbody performance. A strut-mounted cone-cylinder model with three separate afterbody configurations for Aerospace Research and Development (AGARD) was used for this investigation. This program was conducted in two phases distinguished by the model size and the wind tunnels used to obtain the experimental results. The effect of tunnel wall porosity on nozzle afterbody (NAB) performance was investigated.
Book Synopsis Subject, Author & Paper Number Cumulative Index to Transactions of the ASME, 1971/1975 by : American Society of Mechanical Engineers
Download or read book Subject, Author & Paper Number Cumulative Index to Transactions of the ASME, 1971/1975 written by American Society of Mechanical Engineers and published by . This book was released on 1976 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low Reynolds Number Nozzle Flow Study by : Margaret V. Whalen
Download or read book Low Reynolds Number Nozzle Flow Study written by Margaret V. Whalen and published by . This book was released on 1987 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Standardized Nozzles and Orifices Used in Closed Conduits Results of Experiments at Low Reynolds Numbers by : Mario Marchetti
Download or read book Standardized Nozzles and Orifices Used in Closed Conduits Results of Experiments at Low Reynolds Numbers written by Mario Marchetti and published by . This book was released on 1939 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Effect of Reynolds Number on Efficiencies and Velocity Coefficients of Very Small Supersonic Air Nozzles by : Thomas Peters Kennedy
Download or read book Experimental Investigation of the Effect of Reynolds Number on Efficiencies and Velocity Coefficients of Very Small Supersonic Air Nozzles written by Thomas Peters Kennedy and published by . This book was released on 1952 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer and Flow Characteristics of Sonic Nozzle by : Ganapathi Reddy Madamadakala
Download or read book Heat Transfer and Flow Characteristics of Sonic Nozzle written by Ganapathi Reddy Madamadakala and published by . This book was released on 2013 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: The current research presents the experimental investigation of heat transfer and flow characteristics of sonic multiphase flow in a converging-diverging nozzle. R134a and R123 are used in this study. Four different nozzle assemblies with two different throat sizes (2.43mm and 1.5 mm with 1° growth angle with the centerline of the nozzle in the diverging section) and two different heater lengths (200 mm and 125 mm) were tested. Each test section was an assembly of aluminum nozzle sections. The experimental facility design allowed controlling three variables: throat velocity, inlet temperature, back pressure saturation temperature. The analysis used to find the average heat transfer of the fluid to each nozzle section. This was achieved by measuring the nozzle wall temperature and fluid pressure in a steady state condition. Two methods for finding the average heat flux in sonic nozzle were included in the data analysis: infinite contact resistance and zero contact resistance between nozzle sections. The input variables ranges were 25°C and 30°C for inlet temperature and back pressure saturation temperatures, 1100-60,000 kg/m2s for mass flux, and 1.4-700 kW/m2 heat flux. The effect of the mass flux and heat flux on the average two-phase heat transfer coefficients was investigated. The flow quality, Mach number(M), and Nusselt number ratio ([phi]) were also calculated for each section of the nozzle. As the fluid flowed through the nozzle, the pressure of the liquid dropped below the inlet saturation pressure of the liquid due to sonic expansion in the nozzle. This temperature drop was significantly lower in the case of R134a than R123. The results showed that the two-phase heat transfer coefficients were above of 30000 W/m^2 K in the first 75 mm of the nozzle, and they decreased along the nozzle. The Mach number profile appeared similar to the temperature profile, and the fluid was in the sonic region as long as temperature of the fluid dropped in the nozzle. Nusselt number ratios were compared with the Mach numbers and showed that the Nusselt number ratio were increased in the sonic region. The results showed that the length of the sonic region was larger for R123 than for R134a, and the Mach numbers were higher for R123. The Nusselt ratios of R123 were low compared to the R134a cases, and the trend in the Nusselt ratios was notably different as well.
Book Synopsis The Effect of Viscosity on the Discharge Coefficients of Square-edged Orifices by : Charles C. Watson
Download or read book The Effect of Viscosity on the Discharge Coefficients of Square-edged Orifices written by Charles C. Watson and published by . This book was released on 1933 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
