Calculation of the Downwash Behind Sweptback Wings - Part 2
| Author | : H. Schlichting |
| Publisher | : |
| Total Pages | : 25 |
| Release | : 1947 |
| Genre | : |
| ISBN | : |
Download Calculation of the Downwash Behind Sweptback Wings - Part 2 Book in PDF, Epub and Kindle
Calculation Of The Downwash Behind Sweptback Wings Part 2
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Calculation of the Downwash Behind Sweptback Wings
| Author | : H. Schlichting |
| Publisher | : |
| Total Pages | : 14 |
| Release | : 1947 |
| Genre | : |
| ISBN | : |
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Calculation of Downwash Behind a Swept-back Wing
| Author | : Paul G. Johnson |
| Publisher | : |
| Total Pages | : 41 |
| Release | : 1948 |
| Genre | : |
| ISBN | : |
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The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms
| Author | : Maxwell Alfred Heaslet |
| Publisher | : |
| Total Pages | : 52 |
| Release | : 1948 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
Download The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms Book in PDF, Epub and Kindle
A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Damping-in-roll Calculations for Slender Swept-back Wings and Slender Wing-body Combinations
| Author | : Harvard Lomax |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1949 |
| Genre | : Aerofoils |
| ISBN | : |
Download Damping-in-roll Calculations for Slender Swept-back Wings and Slender Wing-body Combinations Book in PDF, Epub and Kindle
The damping-in-roll parameter C(iota)(p) is calculated theoretically for triangular wings on cylindrical bodies and for a class of wings with sweptback plan forms. The analysis is based on the usual assumptions of linearized compressible-flow theory together with the added restrictions that at the free-stream Mach number M(omicron) the product of lM(omicron)(2) and the streamwise velocity gradient is small.
Summary and Analysis of Horizontal-tail Contribution to Longitudinal Stability of Swept-wing Airplanes at Low Speeds
| Author | : Robert H. Neely |
| Publisher | : |
| Total Pages | : 100 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
Download Summary and Analysis of Horizontal-tail Contribution to Longitudinal Stability of Swept-wing Airplanes at Low Speeds Book in PDF, Epub and Kindle
Air-flow characteristics behind wings and wing-body combinations are described and are related to the downwash at specific tail locations for unseparated and separated flow conditions. The effects of various parameters and control devices on the air-flow characteristics and tail contribution are analyzed and demonstrated. An attempt has been made to summarize certain data in a form useful for design. The experimental data herein were obtained mostly at Reynolds numbers greater than 4 x 105 and at Mach numbers less than 0.25.
Downwash, Sidewash, and Wave Survey Behind a 420 Sweptback Wing at a Reynolds Number of 6.8 X 106 with and Without a Simulated Ground
| Author | : G. Chester Furlong |
| Publisher | : |
| Total Pages | : 82 |
| Release | : 1948 |
| Genre | : Aiprlanes |
| ISBN | : |
Download Downwash, Sidewash, and Wave Survey Behind a 420 Sweptback Wing at a Reynolds Number of 6.8 X 106 with and Without a Simulated Ground Book in PDF, Epub and Kindle
A Method of Calculation of Downwash Behind a Swept Wing
| Author | : Austin H. Gale |
| Publisher | : |
| Total Pages | : 62 |
| Release | : 1949 |
| Genre | : |
| ISBN | : |
Download A Method of Calculation of Downwash Behind a Swept Wing Book in PDF, Epub and Kindle
Theoretical and Experimental Investigation of the Subsonic-flow Fields Beneath Swept and Unswept Wings with Tails of Vortex-induced Velocities
| Author | : William J. Alford |
| Publisher | : |
| Total Pages | : 100 |
| Release | : 1956 |
| Genre | : Air flow |
| ISBN | : |
Download Theoretical and Experimental Investigation of the Subsonic-flow Fields Beneath Swept and Unswept Wings with Tails of Vortex-induced Velocities Book in PDF, Epub and Kindle
The flow-field characteristics beneath swept and unswept wings as determined by potential-flow theory are compared with the experimentally determined flow fields beneath swept and unswept wing-fuselage combinations. The potential-flow theory utilized considered both the spanwise and chordwise distributions of vorticity as well as the wing-thickness effects. The perturbation velocities induced by a unit horseshoe vortex are included in tabular form.
