[PDF] Experimental Investigation Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities - eBooks Review

Experimental Investigation Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities


Experimental Investigation Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities
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Experimental Investigation Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities


Experimental Investigation Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities
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Author : Dean R. Chapman
language : en
Publisher:
Release Date : 1952

Experimental Investigation Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities written by Dean R. Chapman 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.


The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.



Report


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

Report 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.




Annual Report Of The National Advisory Committee For Aeronautics


Annual Report Of The National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954

Annual Report Of The 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 1954 with Aeronautics categories.


Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.



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 : 1956

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 1956 with Aeronautics categories.




Report National Advisory Committee For Aeronautics


Report National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1952

Report 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 1952 with Aeronautics categories.




An Empirically Derived Basis For Calculating The Area Rate And Distribution Of Water Drop Impingement On Airfoils


An Empirically Derived Basis For Calculating The Area Rate And Distribution Of Water Drop Impingement On Airfoils
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Author : Antonio Ferri
language : en
Publisher:
Release Date : 1952

An Empirically Derived Basis For Calculating The Area Rate And Distribution Of Water Drop Impingement On Airfoils written by Antonio Ferri and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aerodynamic load categories.




Afterbody Pressures On Two Dimensional Boattailed Bodies Having Turbulent Boundary Layers At Mach 5 98


Afterbody Pressures On Two Dimensional Boattailed Bodies Having Turbulent Boundary Layers At Mach 5 98
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Author : W. Frank Staylor
language : en
Publisher:
Release Date : 1964

Afterbody Pressures On Two Dimensional Boattailed Bodies Having Turbulent Boundary Layers At Mach 5 98 written by W. Frank Staylor and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aerodynamics, Transonic categories.




Nasa Technical Note


Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1973

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with categories.




Applied Mechanics Reviews


Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1965

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 1965 with Mechanics, Applied categories.




Naca Research Memorandum


Naca Research Memorandum
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Author :
language : en
Publisher:
Release Date : 19??

Naca Research Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 19?? with Aerodynamics categories.