Ideal Gas Tables For Oblique Shock Flow Parameters In Air At Mach Numbers From 1 05 To 12 0

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Ideal Gas Tables For Oblique Shock Flow Parameters In Air At Mach Numbers From 1 05 To 12 0
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Author : John S. Dennard
language : en
Publisher:
Release Date : 1964
Ideal Gas Tables For Oblique Shock Flow Parameters In Air At Mach Numbers From 1 05 To 12 0 written by John S. Dennard and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aeronautics categories.
Oblique-shock tables are presented for air with initial Mach numbers from 1.05 to 12.0 and flow-deflection angles from 0 degrees up to the maximum turning angle for attached flow. Parameters presented are flow-deflection angle, shock-wave angle, total-pressure ratio, static-pressure, density, and temperature ratios, downstream Mach number, ratio of downstream velocity to maximum velocity, and increase in entropy. Perfect-gas equations have been used throughout these calculations.
The Correlation Of Oblique Shock Parameters For Ratios Of Specific Heats From 1 To 5 3 With Application To Real Gas Flows
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Author : Mitchel H. Bertram
language : en
Publisher:
Release Date : 1963
The Correlation Of Oblique Shock Parameters For Ratios Of Specific Heats From 1 To 5 3 With Application To Real Gas Flows written by Mitchel H. Bertram and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Gas flow categories.
An analytic investigation was made to show the extent of correlation of the exact oblique shock parameters that may be accomplished by means of similarity parameters suggested by approximate theory. The exact theory for the inviscid flow of a perfect gas was calculated for Mach numbers of 1.1 to 40, ratios of specific heats from 1 to 5/3, and angles of attack from 0° to shock detachment. From consideration of the approximate theory and the concept of effective ratio of specific heats, the oblique shock correlations were found to be useful for the rapid calculation of many flow parameters for an equilibrium real gas. Some useful correlations are also given for the case of isentropic expansion around a sharp corner.
Charts And Approximate Formulas For The Estimation Of Aeroelastic Effects On The Lateral Control Of Swept And Unswept Wings
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Author : Almer D. Crim
language : en
Publisher:
Release Date : 1952
Charts And Approximate Formulas For The Estimation Of Aeroelastic Effects On The Lateral Control Of Swept And Unswept Wings written by Almer D. Crim and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aerodynamics, Supersonic categories.
Shock Waves In Real Gases
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Author :
language : en
Publisher:
Release Date : 1969
Shock Waves In Real Gases written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Gas dynamics categories.
Fox And Mcdonald S Introduction To Fluid Mechanics
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Author : Philip J. Pritchard
language : en
Publisher: John Wiley & Sons
Release Date : 2016-05-23
Fox And Mcdonald S Introduction To Fluid Mechanics written by Philip J. Pritchard and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2016-05-23 with Science categories.
Fox & McDonald’s Introduction to Fluid Mechanics 9th Edition has been one of the most widely adopted textbooks in the field. This highly-regarded text continues to provide readers with a balanced and comprehensive approach to mastering critical concepts, incorporating a proven problem-solving methodology that helps readers develop an orderly plan to finding the right solution and relating results to expected physical behavior. The ninth edition features a wealth of example problems integrated throughout the text as well as a variety of new end of chapter problems.
Semiempirical Method For Predicting Effects Of Incident Reflecting Shocks On The Turbulent Boundary Layer
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Author : Shimer Zane Pinckney
language : en
Publisher:
Release Date : 1965
Semiempirical Method For Predicting Effects Of Incident Reflecting Shocks On The Turbulent Boundary Layer written by Shimer Zane Pinckney and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Hypersonic planes categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1994
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aeronautics categories.
Nasa Scientific And Technical Reports
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Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1965
Nasa Scientific And Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aeronautics categories.
Technical Abstract Bulletin
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1961-07
Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961-07 with Technology categories.
Journal Of The British Interplanetary Society
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Author : British Interplanetary Society
language : en
Publisher:
Release Date : 1965
Journal Of The British Interplanetary Society written by British Interplanetary Society and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Astronautics categories.