Download or read book Boundary layer Similar Solutions and Correlation Equations for Laminar Heat transfer Distribution in Equilibrium Air at Velocities Up to 41 100 Feet Per Second written by Nathaniel B. Cohen and published by . This book was released on 1961 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: Correlations of the transport property estimates of NASA TR R-50 are employed to determine locally similar solutions of the laminar boundary-layer equations for air in chemical equilibrium. Exact solutions for flat-plate flow, axisymmetric stagnation flow, and stagnation flow for yawed infinite cylinder are obtained, and a correlation formula for the heat-transfer distribution function for arbitrary favorable pressure gradient is determined. Extension to three-dimensional flows with small cross flow is briefly described.
Download or read book Boundary layer Similar Solutions and Correlation Equations for Laminar Heat transfer Distribution in Equilibrium Air at Velocities Up to 41 100 Feet Per Second written by Nathaniel B. Cohen and published by . This book was released on 1961 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Boundary layer Similar Solutions and Correlation Equations for Laminar Heat transfer Distribution in Equilibrium Air at Velocities Up to 41 100 Feet Per Second written by Nathaniel B. Cohen and published by . This book was released on 1961 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Boundary layer Similar Solutions and Correlation Equations for Laminar Heat transfer Distribution in Equilibrium Air at Velocities Up to 41 000 Feet Per Second written by Nathaniel B. Cohen and published by . This book was released on 1961 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Boundary layer Similar Solutions and Correlation Equations for Laminar Heat Transfer Distributions in Equilibrium Air Velocities Up to 41 100 Feet Per Second with List of References written by and published by . This book was released on 1963 with total page 4 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Boundary layer Similar Solutions and Correlation Equations for Laminar Heat transfer Distribution in Equilibrium Ait at Velocities Up to 41 100 Feet Per Second written by Nathaniel B. Cohen and published by . This book was released on 1963 with total page 57 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 1971 with total page 520 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Approximate Relations for Laminar Heat transfer and Shear stress Functions in Equilibrium Dissociated Air written by Ernest V. Zoby and published by . This book was released on 1968 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Prediction of Aerodynamic Heating of Fins on Re entry Vehicles written by E. C. Lemmon and published by . This book was released on 1971 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Proceedings of Retardation and Recovery Symposium written by and published by . This book was released on 1963 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains the proceedings of the Retardation and Recovery Symposium sponsored by the Aeronautical Systems Division on 13 and 14 November 1962. The Introductory Session was opened with the Keynote Address which reviewed the use and applications of deployable aerodynamic decelerators throughout the past fifty (50) years and noted the areas in which additional work had to be accomplished. The four Technical Sessions deal with the latest significant developments in the retardation and recovery area. The Technical Sessions begin with presentations and discussions of investigations in the hypersonic and supersonic flight regimes followed by a technical analysis of transonic and supersonic flow phenomena. In addition, new aerodynamic decelerator designs and discussion of the wind tunnel tests pertaining to these designs, as well as overall reliability of recovery systems, are presented. The final Technical Session concludes with a discussion of the military, scientific, and general objectives for decelerators intended for future use.
Download or read book Application of Similar Solutions to Calculation of Laminar Heat Transfer on Bodies with Yaw and Large Pressure Gradient in High speed Flow written by Ivan E. Beckwith and published by . This book was released on 1961 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Research Report Avco Everett Research Laboratory written by Avco Corporation. Everett Research Laboratory and published by . This book was released on 1963 with total page 978 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Solution of the Laminar boundary layer Equation for the Flat Plate for Velocity and Temperature Fields for Variable Physical Properties and for the Diffusion Field at High Concentration written by H. Shuh and published by . This book was released on 1950 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: In connection with Pohlhausen's solution for the temperature field on the flat plate, a series of formulas were indicated by means of which the velocity and temperature field for variable physical characteristics can be computed by an integral equation and an iteration method based on it. With it, the following cases were solved: On the assumption that the viscosity simply varies with the temperature while the other fluid properties remain constant, the velocity and temperature field on the heated and cooled plate, respectively, was computed at the Prandtl numbers 12.5 and 100 (viscous fluids). A closer study of these two cases resulted in general relations: The calculations for a gas of Pr number 0.7 (air) were conducted on the assumption that all fluid properties vary with the temperature, and the velocities are low enough for the heat of friction to be discounted. The result was a thickening of the boundary layers, but no appreciable modification in shearing stress or heat-transfer coefficient.
Download or read book Correlation Formulas and Tables of Density and Some Transport Properties of Equilibrium Dissociating Air for Use in Solutions of the Boundary layer Equations written by Nathaniel Bernard Cohen and published by . This book was released on 1960 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Collection of Technical Papers on Guidance Theory and Flight Mechanics written by and published by . This book was released on 1969 with total page 418 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1962 with total page 540 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Real air Data reduction Procedures Based on Flow Parameters Measured in the Test Section of Supersonic and Hypersonic Facilities written by Charles George Miller and published by . This book was released on 1972 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
