Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Effect Of Body Mounted Lateral Controls And Speed Brakes On The Aerodynamic Load Distribution Over A 45 Degree Swept Wing At Mach Numbers From 080 To 098 PDF full book. Access full book title Effect Of Body Mounted Lateral Controls And Speed Brakes On The Aerodynamic Load Distribution Over A 45 Degree Swept Wing At Mach Numbers From 080 To 098.
| Author | : F. E. West |
| Publisher | : |
| Total Pages | : 76 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 80 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
| Author | : F. E. West |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
| Author | : F. E. West |
| Publisher | : |
| Total Pages | : 72 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
| Author | : F. E. West |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1956 |
| Genre | : Airplanes |
| ISBN | : |
An investigation has been made in the Langley 16-foot transonic tunnel to determine the aerodynamic characteristics of several body-mounted lateral-control and speed-brake configurations. The basic model had a 45 degree swept wing with an aspect ratio of 3. Six-component balance data were obtained at Mach numbers of 0.80, 0.94, and 0.98 for angles of attack that usually ranged from about zero to 21 degrees.
| Author | : F. E. West |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1956 |
| Genre | : Aerodynamics, Transonic |
| ISBN | : |
| Author | : Donald E. Hewes |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1951 |
| Genre | : Airplanes |
| ISBN | : |
The trends in lateral stability and control produced variations of the mass distribution were determined for a model with a 45 degree sweptback wing. Calculations were made to correlate the trends determined by theory with those determined from tests of a free-flying dynamic model in the Langley free-flight tunnel.
| Author | : Maurice O. Feryn |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1966 |
| Genre | : |
| ISBN | : |
| Author | : Gerald V. Foster |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1960 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
| Author | : W. F. Lindsey |
| Publisher | : |
| Total Pages | : 24 |
| Release | : 1954 |
| Genre | : Aerodynamics |
| ISBN | : |
Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.
