Investigation Of A Slat In Several Different Positions On An Naca 64a010 Airfoil For A Wide Range Of Subsonic Mach Numbers
DOWNLOAD
Download Investigation Of A Slat In Several Different Positions On An Naca 64a010 Airfoil For A Wide Range Of Subsonic Mach Numbers PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Investigation Of A Slat In Several Different Positions On An Naca 64a010 Airfoil For A Wide Range Of Subsonic Mach Numbers book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Investigation Of A Slat In Several Different Positions On An Naca 64a010 Airfoil For A Wide Range Of Subsonic Mach Numbers
DOWNLOAD
Author : John A. Axelson
language : en
Publisher:
Release Date : 1954
Investigation Of A Slat In Several Different Positions On An Naca 64a010 Airfoil For A Wide Range Of Subsonic Mach Numbers written by John A. Axelson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamics categories.
An investigation of the two-dimensional aerodynamic characteristics of an NACA 64A010 airfoil with a slat has been conducted in the Mach number range from 0.25 to 0.85, with a corresponding Reynolds number range from 3.4 million to 8.1 million. Two families of slat positions were investigated, one with the slat leading edge extended forward along the airfoil chord line, and the other with the slat extended forward and displaced below the chord line.
Technical Note National Advisory Committee For Aeronautics
DOWNLOAD
Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
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 1954 with Aeronautics categories.
Technical Note
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1954
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 1954 with Aeronautics categories.
U S Government Research Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1954
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 1954 with Science categories.
Applied Computational Aerodynamics
DOWNLOAD
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.
Bibliography Of Technical Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1954
Bibliography Of Technical 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 1954 with Science categories.
Aerodynamic Loads On A Leading Edge Flap And A Leading Edge Slat On The Naca 64a010 Airfoil Section
DOWNLOAD
Author : John A. Kelly
language : en
Publisher:
Release Date : 1954
Aerodynamic Loads On A Leading Edge Flap And A Leading Edge Slat On The Naca 64a010 Airfoil Section written by John A. Kelly and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamic load categories.
A previous report, NACA TN 3007, gave force and moment data for the NACA 64A010 airfoil section equipped alternately with a flap and a slat at the leading edge, and with a split flap and a double-slotted flap at the trailing edge. The present report presents the chordwise distributions of pressure measured concurrently with the force and moment data of NACA 3007. The pressure data for the leading-edge flap and slat have been converted into coefficients of normal force, chord force, and moment based on the geometry of the leading-edge device.
Research Abstracts
DOWNLOAD
Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date :
Research Abstracts 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 with Aeronautics categories.
Index Of Naca Technical Publications
DOWNLOAD
Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
Index Of Naca Technical Publications 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.
A Selected Listing Of Nasa Scientific And Technical Reports For
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1949
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 1949 with Aeronautics categories.