Effects Of Two Leading Edge Modifications On The Aerodynamic Characteristics Of A Thin Low Aspect Ratio Delta Wing At Transonic Speeds
![Effects Of Two Leading Edge Modifications On The Aerodynamic Characteristics Of A Thin Low Aspect Ratio Delta Wing At Transonic Speeds](https://ardhindie.com/assets/pdf.png)
DOWNLOAD
Download Effects Of Two Leading Edge Modifications On The Aerodynamic Characteristics Of A Thin Low Aspect Ratio Delta Wing At Transonic Speeds PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Effects Of Two Leading Edge Modifications On The Aerodynamic Characteristics Of A Thin Low Aspect Ratio Delta Wing At Transonic Speeds 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
Effects Of Two Leading Edge Modifications On The Aerodynamic Characteristics Of A Thin Low Aspect Ratio Delta Wing At Transonic Speeds
DOWNLOAD
Author : John P. Mugler
language : en
Publisher:
Release Date : 1956
Effects Of Two Leading Edge Modifications On The Aerodynamic Characteristics Of A Thin Low Aspect Ratio Delta Wing At Transonic Speeds written by John P. Mugler and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamics, Transonic categories.
An investigation was conducted in the Langley 8-foot transonic tunnel to determine the aerodynamic characteristics of a thin 60 degree delta wing with two leading-edge modifications (conical leading-edge camber and leading-edge droop) in combination with bodies with and without body indentation in accordance with the transonic-area-rule concept. The tests covered a Mach number range from 060 to 1.15 and an angle-of-attack range from -4 to 20 degrees at a Reynolds number of about 3,000,000 based on the wing mean aerodynamic chord. The wing had an aspect ratio of 2.31, a taper ratio of 0, and, without modifications, had NACA 65A003 airfoil sections parallel to the model plane of symmetry.
Index Of Nasa Technical Publications
DOWNLOAD
Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960
Index Of Nasa 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 Aeronautics categories.
A Note On The Drag Due To Lift Of Delta Wings At Mach Numbers Up To 2 0
DOWNLOAD
Author : Robert S. Osborne
language : en
Publisher:
Release Date : 1960
A Note On The Drag Due To Lift Of Delta Wings At Mach Numbers Up To 2 0 written by Robert S. Osborne and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aerodynamics categories.
A Note On The Drag Due To Lift Of Delta Wings At Mach Numbers Up To 2 0
DOWNLOAD
Author : Robert S. Osborne
language : en
Publisher:
Release Date : 1953
A Note On The Drag Due To Lift Of Delta Wings At Mach Numbers Up To 2 0 written by Robert S. Osborne and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Airplanes categories.
Nasa Technical Note
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1960
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 1960 with categories.
Aerodynamic Characteristics Of A Delta Wing With Leading Edge Swept Back 45 Degrees Aspect Ratio 4 And Naca 65a006 Airfoil Section
DOWNLOAD
Author : William C. Sleeman
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Delta Wing With Leading Edge Swept Back 45 Degrees Aspect Ratio 4 And Naca 65a006 Airfoil Section written by William C. Sleeman 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.
This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.
Monthly Catalog Of United States Government Publications
DOWNLOAD
Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1959
Monthly Catalog Of United States Government Publications written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Government publications categories.
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Pressure Measurements Obtained In Flight At Transonic Speeds For A Conically Cambered Delta Wing
DOWNLOAD
Author : Earl R. Keener
language : en
Publisher:
Release Date : 1959
Pressure Measurements Obtained In Flight At Transonic Speeds For A Conically Cambered Delta Wing written by Earl R. Keener and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamic load categories.
Index Of Naca Technical Publications
DOWNLOAD
Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1959
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 1959 with Aeronautics categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1954
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 1954 with Aeronautics categories.