Download or read book Hypersonic Shock heated Flow Parameters for Velocities to 46 000 Feet Per Second and Altitudes to 323 000 Feet written by Paul William Huber and published by . This book was released on 1963 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt: Real-air hypersonic-flow parameters are presented in tabular and graphical form for flight in the earth's atmosphere as a function of flight velocity and flight altitude. Thermochemical equilibrium-flow properties are given for the inviscid normal shock and stagnation point, and both equilibrium and frozen-flow parameters, including electron concentration, are listed for the far wake of the inviscid stagnation streamline. Plots of electron collision frequency and electrical conductivity in the normal shock and wake plasmas are also included. The tabulations are made for twelve flight altitudes, ranging from 35,900 feet to 322,900 feet and for flight velocities and shock-heated gas temperatures encompassing those encountered in return from planetary missions. Included are discussions of the applicability of the computed parameters to a given problem, and effects due to the uncertainties in the input data for ambient air.

Download or read book Hypersonic Shock heated Flow Parameters for Velocities to 46 000 Feet Per Second and Altitudes to 323 000 Feet with List of References written by and published by . This book was released on 1963 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Hypersonic Shock heated Flow Parameters for Velocities to 46 000 Feet Per Second and Altitudes to 323 000 Feet written by Paul William Huber and published by . This book was released on 1963 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Hypersonic shook heated flow parameters for velocities to 46 000 feet per second and altitudes to 323 000 feet written by Paul William Huber and published by . This book was released on with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Technical Report written by and published by . This book was released on 1963 with total page 722 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50 000 Per Second 15 24 Kilometers Per Second written by Ernest V. Zoby and published by . This book was released on 1967 with total page 58 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 1968 with total page 416 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Charts of Equilibrium Real gas Stagnation Point Conditions on a Sphere for Altitudes to 200 000 Feet and Velocities to 15 000 Feet Per Second written by P. D. Fisher and published by . This book was released on 1964 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents in graphical form the stagnation point pressure, temperature, equilibrium surface temperature, and heating rate for a sphere. Equilibrium real-gas effects and surface radiation are considered. The charts cover a range of velocities from 0 to 15,000 feet per second and altitudes from sea level to 200,000 feet. Corrections for sphere diameter and emissivity are included. (Author).

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1964 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Flight Measurement of Optical Radiation from Shock heated Air by Using a Trailblazer II Vehicle written by Lloyd S. Keafer and published by . This book was released on 1968 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Hypersonic and High Temperature Gas Dynamics written by John David Anderson and published by AIAA. This book was released on 1989 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.

Download or read book Computational Aerodynamic Modeling of Aerospace Vehicles written by Mehdi Ghoreyshi and published by MDPI. This book was released on 2019-03-08 with total page 294 pages. Available in PDF, EPUB and Kindle. Book excerpt: Currently, the use of computational fluid dynamics (CFD) solutions is considered as the state-of-the-art in the modeling of unsteady nonlinear flow physics and offers an early and improved understanding of air vehicle aerodynamics and stability and control characteristics. This Special Issue covers recent computational efforts on simulation of aerospace vehicles including fighter aircraft, rotorcraft, propeller driven vehicles, unmanned vehicle, projectiles, and air drop configurations. The complex flow physics of these configurations pose significant challenges in CFD modeling. Some of these challenges include prediction of vortical flows and shock waves, rapid maneuvering aircraft with fast moving control surfaces, and interactions between propellers and wing, fluid and structure, boundary layer and shock waves. Additional topic of interest in this Special Issue is the use of CFD tools in aircraft design and flight mechanics. The problem with these applications is the computational cost involved, particularly if this is viewed as a brute-force calculation of vehicle’s aerodynamics through its flight envelope. To make progress in routinely using of CFD in aircraft design, methods based on sampling, model updating and system identification should be considered.

Download or read book Calculated Radio Attenuation Due to Plasma Sheath on Hypersonic Blunt nosed Cone written by John S. Evans and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1964 with total page 1156 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1965 with total page 1152 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book High Enthalpy Gas Dynamics written by Ethirajan Rathakrishnan and published by John Wiley & Sons. This book was released on 2014-12-22 with total page 352 pages. Available in PDF, EPUB and Kindle. Book excerpt: This is an introductory level textbook which explains the elements of high temperature and high-speed gas dynamics. written in a clear and easy to follow style, the author covers all the latest developments in the field including basic thermodynamic principles, compressible flow regimes and waves propagation in one volume covers theoretical modeling of High Enthalpy Flows, with particular focus on problems in internal and external gas-dynamic flows, of interest in the fields of rockets propulsion and hypersonic aerodynamics High enthalpy gas dynamics is a compulsory course for aerospace engineering students and this book is a result of over 25 years' teaching by the author accompanying website includes a Solutions Manual for exercises listed at the end of each chapter, plus lecture slides

Download or read book Hypersonic Aerothermodynamics written by John J. Bertin and published by AIAA. This book was released on 1994 with total page 644 pages. Available in PDF, EPUB and Kindle. Book excerpt: A modern treatment of hypersonic aerothermodynamics for students, engineers, scientists, and program managers involved in the study and application of hypersonic flight. It assumes an understanding of the basic principles of fluid mechanics, thermodynamics, compressible flow, and heat transfer. Ten chapters address: general characterization of hypersonic flows; basic equations of motion; defining the aerothermodynamic environment; experimental measurements of hypersonic flows; stagnation-region flowfield; the pressure distribution; the boundary layer and convective heat transfer; aerodynamic forces and moments; viscous interactions; and aerothermodynamics and design considerations. Includes sample exercises and homework problems. Annotation copyright by Book News, Inc., Portland, OR