Ordinates And Theoretical Pressure Distribution Data For Naca 6 And 6a Series Airfoil Sections With Thicknesses From 2 To 21 And From 2 To 15 Percent Chord Respectively
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Ordinates And Theoretical Pressure Distribution Data For Naca 6 And 6a Series Airfoil Sections With Thicknesses From 2 To 21 And From 2 To 15 Percent Chord Respectively
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Author : Elizabeth W. Patterson
language : en
Publisher:
Release Date : 1961
Ordinates And Theoretical Pressure Distribution Data For Naca 6 And 6a Series Airfoil Sections With Thicknesses From 2 To 21 And From 2 To 15 Percent Chord Respectively written by Elizabeth W. Patterson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerofoils categories.
Summary: Basic thickness forms of the NACA 63-, 64-, 65- series and NACA 63A-, 64A-, 65 A-series airfoil sections are tabulated for thicknesses of 2, 3, 4, and 5 percent chord. Also presented for these thin airfoil sections are theoretical values of pressures and velocity ratios required to obtain theoretical airfoil pressure distributions. In addition, for each family of airfoil sections, cross plots are presented from which ordinates and pressure distributions can be easily obtained for airfoil sections of thicknesses intermediate to those presented in this report, in NACA Report 824 (from 6 to 21 percent chord for the NACA 6-series), and in NACA Report 903 (from 6 to 15 percent chord for the NACA 6A-series).
Ordinates And Theoretical Pressure Distribution Data For Naca 6 And 6a Series Airfoil Sections With Thicknesses From 2 To 21 And From 2 To 15 Percent Chord Respectively
DOWNLOAD
Author : Elizabeth W. Patterson
language : en
Publisher:
Release Date : 1958
Ordinates And Theoretical Pressure Distribution Data For Naca 6 And 6a Series Airfoil Sections With Thicknesses From 2 To 21 And From 2 To 15 Percent Chord Respectively written by Elizabeth W. Patterson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Aerofoils categories.
Basic thickness forms of the NACA 63-, 64-, 65-series and NACA 63A-, 64A-, 65A-series airfoil sections are tabulated for thicknesses of 2, 3, 4, and 5 percent chord. Also presented for these thin airfoil sections are theoretical values of pressures and velocity ratios required to obtain theoretical airfoil pressure distributions. In addition, for each fsmily of airfoil sections, cross plots are presented from which ordinates and pressure distributions can be easily obtained for airfoil sections of thicknesses intermediate to those presented in this report, in NACA Report 824 (from 6 to 21 percent chord for the NACA 6-series), and in NACA Report 903 (from 6 to 15 percent chord for the NACA 6A-series).
Ordinates And Theoretical Pressure Distribution Data For Naca 6 And 6a Series Airfoil Sections With Thickness From 2 To 21 And From 2 To 15 Percent Chord Respectively
DOWNLOAD
Author : Elizabeth W. Patterson
language : en
Publisher:
Release Date : 1958
Ordinates And Theoretical Pressure Distribution Data For Naca 6 And 6a Series Airfoil Sections With Thickness From 2 To 21 And From 2 To 15 Percent Chord Respectively written by Elizabeth W. Patterson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with categories.
Ordinates And Theoretical Pressure Distribution Data For Naca 6 And 6a Series Airfoil Sections With Thicknesses From 2 To 21 And From 2 To 15 Percent Chord Respectively With List Of References
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Author :
language : en
Publisher:
Release Date : 1961
Ordinates And Theoretical Pressure Distribution Data For Naca 6 And 6a Series Airfoil Sections With Thicknesses From 2 To 21 And From 2 To 15 Percent Chord Respectively With List Of References written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.
Turbojet Engine Noise Reduction With Mixing Nozzle Ejector Combinations
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Author : Willard D. Coles
language : en
Publisher:
Release Date : 1958
Turbojet Engine Noise Reduction With Mixing Nozzle Ejector Combinations written by Willard D. Coles 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.
Several noise suppressors consisting of combinations of mixing nozzles and ejectors were tested on two full-scale turbojet engines. Maximum sound pressure level reductions of 12 decibels and sound power level reductions of 8 decibels were obtained. The ejectors provided 3 to 5 decibels of the sound power reduction. The effects of ejector dimensions on noise suppression and engine performance were investigated. Ejector lengths of approximately 2.0 standard nozzle diameters and ejector diameters larger than 1.6 standard nozzle diameters provided the greatest additional noise reduction to that obtained with the mixing nozzles alone. The ejector can restore the static thrust loss caused by use of the mixing nozzle or can provide static-thrust augmentation.
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.
U S Government Research Reports
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Author :
language : en
Publisher:
Release Date : 1959
U S Government Research 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 1959 with Science categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1960
A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aeronautics categories.
Index Of N A S A Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960
Index Of N A S A Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.
Applied Computational Aerodynamics
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Author : Russell M. Cummings
language : en
Publisher: Cambridge University Press
Release Date : 2015-04-27
Applied Computational Aerodynamics written by Russell M. Cummings and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-04-27 with Mathematics categories.
This book covers the application of computational fluid dynamics from low-speed to high-speed flows, especially for use in aerospace applications.