Effects Of Compressibility On The Maximum Lift Characteristics And Spanwise Load Distribution Of A 12 Foot Span Fighter Type Wing Of Naca 230 Series Airfoil Sections
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Effects Of Compressibility On The Maximum Lift Characteristics And Spanwise Load Distribution Of A 12 Foot Span Fighter Type Wing Of Naca 230 Series Airfoil Sections
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Author : E. O. Pearson
language : en
Publisher:
Release Date : 1945
Effects Of Compressibility On The Maximum Lift Characteristics And Spanwise Load Distribution Of A 12 Foot Span Fighter Type Wing Of Naca 230 Series Airfoil Sections written by E. O. Pearson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1945 with Aerodynamic load categories.
Force and pressure-distribution measurements were made on a fighter-type wing model of conventional NACA 230-series airfoil sections in the Langley 16-foot high-speed tunnel to determine the effects of compressibility on the maximum lift characteristics and the span-wise load distribution. The range of angle of attack investigated was from -10 to +24 degrees. The Mach range of from 0.20 to 0.70 at small and medium angles of attack and from 0.15 to 0.625 at very large angles of attack. Maximum lift coefficient increased up to a Mach number of 0.3, decreased rapidly to a Mach number of 0.55, and then decreased moderately. At high speeds, maximum lift coefficient was reached at from 10 to 12 degrees beyond the stalling angle. In high-speed stalls, resultant load underwent a moderate shift outward.
Effects Of Compressibility On The Maximum Lift Characteristics And Spanwise Load Distribution Of A 12 Foot Span Fighter Type Wing Of Naca 230 Series Airfoil Sections
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Author : Langley Aeronautical Laboratory
language : en
Publisher: Hassell Street Press
Release Date : 2021-09-09
Effects Of Compressibility On The Maximum Lift Characteristics And Spanwise Load Distribution Of A 12 Foot Span Fighter Type Wing Of Naca 230 Series Airfoil Sections written by Langley Aeronautical Laboratory and has been published by Hassell Street Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2021-09-09 with categories.
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Effects Of Compressibility On Lift And Load Characteristics Of A Tapered Wing Of Naca 64 210 Airfoil Sections Up To A Mach Number Of 0 60
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Author : F. E. West
language : en
Publisher:
Release Date : 1949
Effects Of Compressibility On Lift And Load Characteristics Of A Tapered Wing Of Naca 64 210 Airfoil Sections Up To A Mach Number Of 0 60 written by F. E. West and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerofoils categories.
The effects of compressibility on the lift, pressure, pitching-moment, and load characteristics of a 12-foot tapered wing having NACA 64-210 airfoil sections and aspect ratio of 6 is presented for Mach numbers up to 0.60 and an angle-of-attack range of -4 degrees up through the stall.
Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1950
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 1950 with Aeronautics categories.
Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1949
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 1949 with Aeronautics categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
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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.
Technical Note
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Author :
language : en
Publisher:
Release Date : 1947
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 1947 with Aeronautics categories.
Dynamometer Stand Investigation Of The Muffler Used In The Demonstration Of Light Airplane Noise Reduction
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Author : K. R. Czarnecki
language : en
Publisher:
Release Date : 1948
Dynamometer Stand Investigation Of The Muffler Used In The Demonstration Of Light Airplane Noise Reduction written by K. R. Czarnecki and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Airplanes categories.
The attenuation characteristics of the muffler used in the demonstration of light airplane noise reduction were investigated on the ground dynamometer stand at the Langley full-scale tunnel. Sound, back pressure, and engine power output were measured. The ground tests indicated that a reduction of 10 to 15 decibels was to be expected from this muffler.
Wartime Report
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Author :
language : en
Publisher:
Release Date : 194?
Wartime Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 194? with Aeronautics categories.
Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Wartime Report
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date :
Wartime 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 with Aeronautics categories.