Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 35 Aspect Ratio 6 Taper Ratio 0 6 And Naca 65a006 Airfoil Section
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Aerodynamic Characteristics of a Wing with Quarter chord Line Swept Back 35 Aspect Ratio 6 Taper Ratio 0 6 and NACA 65A006 Airfoil Section
Author | : William C. Sleeman |
Publsiher | : Unknown |
Total Pages | : 36 |
Release | : 1949 |
Genre | : Aerodynamics, Transonic |
ISBN | : UOM:39015086464610 |
Download Aerodynamic Characteristics of a Wing with Quarter chord Line Swept Back 35 Aspect Ratio 6 Taper Ratio 0 6 and NACA 65A006 Airfoil Section Book in PDF, Epub and Kindle
Aerodynamic Characteristics of a Wing with Quarter chord Line Swept Back 45 Degrees Aspect Ratio 4 Taper Ratio 0 3 and NACA 65A006 Airfoil Section
Author | : Boyd C. Myers |
Publsiher | : Unknown |
Total Pages | : 36 |
Release | : 1949 |
Genre | : Airplane |
ISBN | : UOM:39015086490524 |
Download Aerodynamic Characteristics of a Wing with Quarter chord Line Swept Back 45 Degrees Aspect Ratio 4 Taper Ratio 0 3 and NACA 65A006 Airfoil Section Book in PDF, Epub and Kindle
This paper presents the results of the investigation of a wing-alone and wing-fuselage configuration employing a wing with the quarter-chord line swept back 45 degrees, with aspect ratio 4, taper ratio 0.3, 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 were also obtained for these configurations and are presented for a range of tail heights at one tail length. In order to expedite the publishing of these data, only a brief analysis is included.
Index of NACA Technical Publications
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 242 |
Release | : 1955 |
Genre | : Aeronautics |
ISBN | : STANFORD:36105024165651 |
Download Index of NACA Technical Publications Book in PDF, Epub and Kindle
A Selected Listing of NASA Scientific and Technical Reports for
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 750 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : UVA:X004173285 |
Download A Selected Listing of NASA Scientific and Technical Reports for Book in PDF, Epub and Kindle
Lateral control Investigation of Flap type Controls on a Wing with Quarter chord Line Sweptback 35 Aspect Ratio 4 Taper Ratio 0 6 and NACA 65A006 Airfoil Section
Author | : Robert F. Thompson |
Publsiher | : Unknown |
Total Pages | : 28 |
Release | : 1950 |
Genre | : Aerofoils |
ISBN | : UOM:39015086490557 |
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This paper presents the results of an investigation to determine the control-effectiveness characteristics of 30-percent-chord flap-type control surfaces of various spans on a semispan wing-fuselage model. The wing of the mode had 35 degrees of sweepback of the quarter chord, an aspect ratio of 4.0, a taper ratio of 0.6, and an NACA 65A006 airfoil section parallel to the free stream. Lift, rolling moments, and pitching moments were obtained for several angle of attack throughout a small range of control-surface deflections. Most of the data are presented as control-effectiveness parameters which show their variation with Mach number.
Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees Aspect Ratio 4 and NACA 65A006 Airfoil Section
Author | : William C. Sleeman |
Publsiher | : Unknown |
Total Pages | : 34 |
Release | : 1949 |
Genre | : Aerofoils |
ISBN | : UOM:39015086464503 |
Download Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees Aspect Ratio 4 and NACA 65A006 Airfoil Section Book in PDF, Epub and Kindle
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.
Research Abstracts and Reclassification Notice
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 508 |
Release | : 1954 |
Genre | : Aeronautics |
ISBN | : IND:30000098603164 |
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Research Abstracts
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 442 |
Release | : 2024 |
Genre | : Aeronautics |
ISBN | : OSU:32435062280326 |
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