Some Theoretical Low Speed Span Loading Characteristics Of Swept Wings In Roll And Sideslip PDF Download
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| Author | : John D. Bird |
| Publisher | : |
| Total Pages | : 44 |
| Release | : 1949 |
| Genre | : Aeronautics |
| ISBN | : |
Download Some Theoretical Low-speed Span Loading Characteristics of Swept Wings in Roll and Sideslip Book in PDF, ePub and Kindle
The 7-point method of Weissinger is used to calculate the span loading in roll, lateral center of pressure, and damping in roll for wings having various aspect ratios, sweep angles, and taper ratios. The applicability of the method to the determination of certain other aerodynamic derivatives is investigated, and corrections for the first-order effects of compressibility are indicated.
| Author | : John D. Bird |
| Publisher | : |
| Total Pages | : 15 |
| Release | : 1950 |
| Genre | : |
| ISBN | : |
Download Some Theoretical Low-speed Span Loading Characteristics of Swept Wings in Roll and Sideslip Book in PDF, ePub and Kindle
| Author | : Edward Charles Polhamus |
| Publisher | : |
| Total Pages | : 86 |
| Release | : 1960 |
| Genre | : Aerodynamics, Transonic |
| ISBN | : |
Download The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds Book in PDF, ePub and Kindle
| Author | : Edward C. Polhamus |
| Publisher | : |
| Total Pages | : 90 |
| Release | : 1955 |
| Genre | : Aerodynamics |
| ISBN | : |
Download The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds Book in PDF, ePub and Kindle
A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1034 |
| Release | : 1953 |
| Genre | : Aeronautics |
| ISBN | : |
Download Technical Note - National Advisory Committee for Aeronautics Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 624 |
| Release | : 1949 |
| Genre | : Aeronautics |
| ISBN | : |
Download Technical Note Book in PDF, ePub and Kindle
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 498 |
| Release | : 1952 |
| Genre | : Aeronautics |
| ISBN | : |
Download Index of NACA Technical Publications Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 664 |
| Release | : 1949 |
| Genre | : Aeronautics |
| ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, ePub and Kindle
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1200 |
| Release | : 1954 |
| Genre | : Aeronautics |
| ISBN | : |
Download Annual Report of the National Advisory Committee for Aeronautics Book in PDF, ePub and Kindle
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
| Author | : John DeYoung |
| Publisher | : |
| Total Pages | : 106 |
| Release | : 1950 |
| Genre | : Aerodynamic load |
| ISBN | : |
Download Theoretical Antisymmetric Span Loading for Wings of Arbitrary Plan Form at Subsonic Speeds Book in PDF, ePub and Kindle
A simplified lifting-surface theory that includes effects of compressibility and spanwise variation of section lift-curve slope is used to provide charts with which antisymmetric loading due to arbitrary antisymmetric angle of attack can be found for wings having symmetric plan forms with a constant spanwise sweep angle of the quarter-chord line. Consideration is given to the flexible wing in roll. Aerodynamic characteristics due to rolling, deflected ailerons, and sideslip of wings with dihedral are considered. Solutions are presented for straight-tapered wings for a range of swept plan forms.
