[PDF] Approximate Turbulent Boundary Layer Development In Plane Compressible Flow Along Thermally Insulated Surfaces With Application To Supersonic Tunnel Contour Correction - eBooks Review

Approximate Turbulent Boundary Layer Development In Plane Compressible Flow Along Thermally Insulated Surfaces With Application To Supersonic Tunnel Contour Correction


Approximate Turbulent Boundary Layer Development In Plane Compressible Flow Along Thermally Insulated Surfaces With Application To Supersonic Tunnel Contour Correction
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Approximate Turbulent Boundary Layer Development In Plane Compressible Flow Along Thermally Insulated Surfaces With Application To Supersonic Tunnel Contour Correction


Approximate Turbulent Boundary Layer Development In Plane Compressible Flow Along Thermally Insulated Surfaces With Application To Supersonic Tunnel Contour Correction
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Author : Maurice Tucker
language : en
Publisher:
Release Date : 1950

Approximate Turbulent Boundary Layer Development In Plane Compressible Flow Along Thermally Insulated Surfaces With Application To Supersonic Tunnel Contour Correction written by Maurice Tucker and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Air flow categories.


As an application of the method, the contour correction of supersonic nozzles for the effects of boundary-layer development is discussed from the requirement of continuity of mass flow and from the requirement of expansion- and shock-wave elimination.



Technical Note National Advisory Committee For Aeronautics


Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1958

Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Aeronautics categories.




Turbulent Flows And Heat Transfer


Turbulent Flows And Heat Transfer
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Author : Chia-Ch'iao Lin
language : en
Publisher: Princeton University Press
Release Date : 2015-12-08

Turbulent Flows And Heat Transfer written by Chia-Ch'iao Lin and has been published by Princeton University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-12-08 with Science categories.


Volume V of the High Speed Aerodynamics and Jet Propulsion series. Topics include transition from laminar to turbulent flow; turbulent flow; statistical theories of turbulence; conduction of heat; convective heat transfer and friction in flow of liquids; convective heat transfer in gases; cooling by protective fluid films; physical basis of thermal radiation; and engineering calculations of radiant heat exchange. Originally published in 1959. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.



Turbulent Flow


Turbulent Flow
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Author : Galen Brandt Schubauer
language : en
Publisher: Princeton University Press
Release Date : 2015-12-08

Turbulent Flow written by Galen Brandt Schubauer and has been published by Princeton University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-12-08 with Science categories.


Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1945. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.



A Method For Measuring The Product Of Inertia And The Inclination Of The Principal Longitudinal Axis Of Inertia Of An Airplane


A Method For Measuring The Product Of Inertia And The Inclination Of The Principal Longitudinal Axis Of Inertia Of An Airplane
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Author : Robert W. Boucher
language : en
Publisher:
Release Date : 1954

A Method For Measuring The Product Of Inertia And The Inclination Of The Principal Longitudinal Axis Of Inertia Of An Airplane written by Robert W. Boucher and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Airplanes categories.


The angle of inclination of the principal axis was found to have probable error of plus or minus 0.17 degrees both from analysis of the error of inertia measurement of the full-scale airplane and from tests with a model having a simple configuration. Analysis showed the probable error of the inertia measurements for the test airplane to be plus or minus1.00, plus or minus 0.49, and plus or minus 0.35 percent of the true moment of inertia about the X, Y, and Z body reference axes, respectively.



Turbulent Boundary Layer Temperature Recovery Factors In Two Dimensional Supersonic Flow


Turbulent Boundary Layer Temperature Recovery Factors In Two Dimensional Supersonic Flow
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Author : Maurice Tucker
language : en
Publisher:
Release Date : 1951

Turbulent Boundary Layer Temperature Recovery Factors In Two Dimensional Supersonic Flow written by Maurice Tucker and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Aerodynamics, Supersonic categories.


An analytical method is presented for obtaining turbulent temperature recovery factors for a thermally insulated surface in supersonic flow. The method is an extension of Squire's analysis for incompressible flow. The boundary layer velocity profile is represented by a power law and a similarity is postulated for squared-velocity the static-temperature-difference profiles.



Applied Mechanics Reviews


Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1952

Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Mechanics, Applied categories.




Handbook Of Supersonic Aerodynamics


Handbook Of Supersonic Aerodynamics
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Author : R. E. Wilson
language : en
Publisher:
Release Date : 1966

Handbook Of Supersonic Aerodynamics written by R. E. Wilson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Heat categories.




Handbook Of Supersonic Aerodynamics


Handbook Of Supersonic Aerodynamics
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Author : Johns Hopkins University. Applied Physics Laboratory
language : en
Publisher:
Release Date : 1966

Handbook Of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aerodynamics, Supersonic categories.




Qualitative Simulator Study Of Longitudinal Stick Forces And Displacements Desirable During Tracking


Qualitative Simulator Study Of Longitudinal Stick Forces And Displacements Desirable During Tracking
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Author : Stanley Faber
language : en
Publisher:
Release Date : 1958

Qualitative Simulator Study Of Longitudinal Stick Forces And Displacements Desirable During Tracking written by Stanley Faber and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Airplanes categories.


In this study in which an airplane simulator with one degree of freedom (pitch) was used, results were determined for three conditions of airplane dynamics. For an undamped natural frequency of 1/2 cps with a damping ratio of 0.18 and for an undamped natural frequency of 1 cps with a damping ratio of 0.11, moderate longitudinal stick forces and displacements were desired.