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Charts For Equilibrium Isentropic Expansion Of Air Behind Shocks Up To 50000 Per Second 1524 Kilometers Per Second
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Book Synopsis Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50,000 Per Second (15.24 Kilometers Per Second) by : Ernest V. Zoby
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:
Book Synopsis Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50,000 Per Second (15.24 Kilometers Per Second) by : Ernest V. Zoby
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 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50 000 Feet Per Second (15.24 Kilometerws Per Second) by : Ernest V. Zoby
Download or read book Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50 000 Feet Per Second (15.24 Kilometerws Per Second) written by Ernest V. Zoby and published by . This book was released on 1967 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Charts for the Analysis of Isentropic One-dimensional Unsteady Expansions in Equilibrium Real Air with Particular Reference to Shock-initiated Flows by : William L. Grose
Download or read book Charts for the Analysis of Isentropic One-dimensional Unsteady Expansions in Equilibrium Real Air with Particular Reference to Shock-initiated Flows written by William L. Grose and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Charts are presented which facilitate the theoretical analysis of certain flow processes involving an unsteady expansion wave in equilibrium real air. The parameters evaluated are related to (a) the velocity change in an unsteady expansion wave, (b) the maximum velocity attainable in a shock-wave--expansion-wave cycle, (c) the time for characteristic traversal through an expansion wave, and (d) the entropy in shock-initiated flows. Such parameters are of particular interest in analysis of the shock-initiated expansion-tube cycle.
Book Synopsis Normal Shock Waves in Air: Equilibrium Composition and Flow Parameters for Velocities from 26,000 to 50,000 Ft/sec by : Paul V. Marrone
Download or read book Normal Shock Waves in Air: Equilibrium Composition and Flow Parameters for Velocities from 26,000 to 50,000 Ft/sec written by Paul V. Marrone and published by . This book was released on 1962 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Table and Charts of Equilibrium Normal-shock and Shock-tube Properties for Pure Carbon Dioxide with Velocities from 1 to 16 Km/sec by : Charles George Miller
Download or read book Table and Charts of Equilibrium Normal-shock and Shock-tube Properties for Pure Carbon Dioxide with Velocities from 1 to 16 Km/sec written by Charles George Miller and published by . This book was released on 1976 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt: Properties include pressure, temperature, density, enthalpy, speed of sound, entropy, molecular weight ratio, isentropic exponent, velocity, and species mole fractions. Incident (moving) shock velocities are varied from 1 to 16 km/sec for a range of initial pressure of 5 N/sq m to 500 kN/sq m. Working charts illustrating idealized shock tube performance with CO2 test gas and heated helium and hydrogen driver gases are also presented.
Book Synopsis Table and Charts of Equilibrium Normal-shock and Shock-tube Properties for Pure Carbon Dioxide with Velocities from 1 to 16 Km/sec by : Charles George Miller
Download or read book Table and Charts of Equilibrium Normal-shock and Shock-tube Properties for Pure Carbon Dioxide with Velocities from 1 to 16 Km/sec written by Charles George Miller and published by . This book was released on 1976 with total page 324 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Extended Hypervelocity Gas Dynamics Charts for Equilibrium Air by : Richard W. Ziemer
Download or read book Extended Hypervelocity Gas Dynamics Charts for Equilibrium Air written by Richard W. Ziemer and published by . This book was released on 1960 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Normal Shock Wave Calculations in Air at Flight Speeds Up to 25,000 Ft./sec by : Charles A. Cook
Download or read book Normal Shock Wave Calculations in Air at Flight Speeds Up to 25,000 Ft./sec written by Charles A. Cook and published by . This book was released on 1962 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: New calculations of the equilibrium gas proper ties behind a normal shock wave are presented based on the 1959 ARDC Model Atmosphere. Graphs of pressure, density, and temperat8re are pre sented for conditions behind a normal shock wave and at the stagnation point following an isen tropic compression, for high altitude hypersonic flight. The regime treated covers altitude from 100,000 feet to 400,000 feet in increments of 2000 feet, and a range of flight speeds from 10,000 to 25,000 feet per second. (Author).
Book Synopsis Extended Hypervelocity Gas Dynamic Charts for Equilibrium Air by : Richard W. Hales
Download or read book Extended Hypervelocity Gas Dynamic Charts for Equilibrium Air written by Richard W. Hales and published by . This book was released on 1960 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Equilibrium Thermodynamic Properties of Air Behind Incident Normal Shock Waves by : Harry J. Davis
Download or read book Equilibrium Thermodynamic Properties of Air Behind Incident Normal Shock Waves written by Harry J. Davis and published by . This book was released on 1965 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: The equilibrium temperature, density, and pressure of air behind incident normal shock waves have been calculated. The resulting tables include the effects of chemical reactions, excitation, dissociation, ionization, van der Waal and Coulomb forces. The tables are presented as functions of the ratio of the density behind the shock wave to the density at standard conditions in steps of 0.2. The temperature behind the shock wave T2 is a parameter which ranges from 2000K to 16,000K in 1000K steps. Two sets of tables, for initial conditions of 273.15 and 300.0K, are presented. The densities of air, as a real and as an ideal gas, are compared. (Author).
Book Synopsis Aeronautical Engineer's Data Book by : Cliff Matthews
Download or read book Aeronautical Engineer's Data Book written by Cliff Matthews and published by Elsevier. This book was released on 2001-10-17 with total page 282 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aeronautical Engineer's Data Bookis an essential handy guide containing useful up to date information regularly needed by the student or practising engineer. Covering all aspects of aircraft, both fixed wing and rotary craft, this pocket book provides quick access to useful aeronautical engineering data and sources of information for further in-depth information. Quick reference to essential data Most up to date information available
Book Synopsis Table and Charts of Equilibrium Normal-shock and Shock-tube Properties for Carbon Dioxide with Velocities from 1 to 16 Km/sec by : Charles G. III. Miller
Download or read book Table and Charts of Equilibrium Normal-shock and Shock-tube Properties for Carbon Dioxide with Velocities from 1 to 16 Km/sec written by Charles G. III. Miller and published by . This book was released on 1963 with total page 314 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables and Charts of Equilibrium Normal Shock and Shock Tube Solutions for Pure CO 2 with Velocities to 16 Km/sec by : Charles G. Miller
Download or read book Tables and Charts of Equilibrium Normal Shock and Shock Tube Solutions for Pure CO 2 with Velocities to 16 Km/sec written by Charles G. Miller and published by . This book was released on 1974 with total page 179 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aircraft Propulsion by : Saeed Farokhi
Download or read book Aircraft Propulsion written by Saeed Farokhi and published by John Wiley & Sons. This book was released on 2014-04-01 with total page 1052 pages. Available in PDF, EPUB and Kindle. Book excerpt: New edition of the successful textbook updated to include new material on UAVs, design guidelines in aircraft engine component systems and additional end of chapter problems Aircraft Propulsion, Second Edition follows the successful first edition textbook with comprehensive treatment of the subjects in airbreathing propulsion, from the basic principles to more advanced treatments in engine components and system integration. This new edition has been extensively updated to include a number of new and important topics. A chapter is now included on General Aviation and Uninhabited Aerial Vehicle (UAV) Propulsion Systems that includes a discussion on electric and hybrid propulsion. Propeller theory is added to the presentation of turboprop engines. A new section in cycle analysis treats Ultra-High Bypass (UHB) and Geared Turbofan engines. New material on drop-in biofuels and design for sustainability is added to refl ect the FAA’s 2025 Vision. In addition, the design guidelines in aircraft engine components are expanded to make the book user friendly for engine designers. Extensive review material and derivations are included to help the reader navigate through the subject with ease. Key features: General Aviation and UAV Propulsion Systems are presented in a new chapter Discusses Ultra-High Bypass and Geared Turbofan engines Presents alternative drop-in jet fuels Expands on engine components' design guidelines The end-of-chapter problem sets have been increased by nearly 50% and solutions are available on a companion website Presents a new section on engine performance testing and instrumentation Includes a new 10-Minute Quiz appendix (with 45 quizzes) that can be used as a continuous assessment and improvement tool in teaching/learning propulsion principles and concepts Includes a new appendix on Rules of Thumb and Trends in aircraft propulsion Aircraft Propulsion, Second Edition is a must-have textbook for graduate and undergraduate students, and is also an excellent source of information for researchers and practitioners in the aerospace and power industry.
Book Synopsis The Tribology Handbook by : Michael J Neale
Download or read book The Tribology Handbook written by Michael J Neale and published by Elsevier. This book was released on 1995-12-15 with total page 577 pages. Available in PDF, EPUB and Kindle. Book excerpt: The renowned reference work is a practical guide to the selection and design of the components of machines and to their lubrication. It has been completely revised for this second edition by leading experts in the area.
Book Synopsis Rocket and Spacecraft Propulsion by : Martin J. L. Turner
Download or read book Rocket and Spacecraft Propulsion written by Martin J. L. Turner and published by Springer Science & Business Media. This book was released on 2006-08-29 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt: The revised edition of this practical, hands-on book discusses the launch vehicles in use today throughout the world, and includes the latest details on advanced systems being developed, such as electric and nuclear propulsion. The author covers the fundamentals, from the basic principles of rocket propulsion and vehicle dynamics through the theory and practice of liquid and solid propellant motors, to new and future developments. He provides a serious exposition of the principles and practice of rocket propulsion, from the point of view of the user who is not an engineering specialist.
