Aeroplanes in Gusts
Author : S. L. Walkden
Publisher :
Page : 278 pages
File Size : 45,94 MB
Release : 1912
Category : Aeronautics
ISBN :
Author : S. L. Walkden
Publisher :
Page : 278 pages
File Size : 45,94 MB
Release : 1912
Category : Aeronautics
ISBN :
Author : Frederic M. Hoblit
Publisher : AIAA
Page : 332 pages
File Size : 19,4 MB
Release : 1988
Category : Airplanes
ISBN : 9781600860607
Author : S. L. Walkden
Publisher :
Page : 280 pages
File Size : 50,38 MB
Release : 1912
Category : Aeronautics
ISBN :
Author : S. L. Walkden
Publisher :
Page : 138 pages
File Size : 45,91 MB
Release : 1914
Category : Aeronautics
ISBN :
Author : Antonio Ferri
Publisher :
Page : 278 pages
File Size : 14,65 MB
Release : 1954
Category : Aerodynamic load
ISBN :
Author : H. Hoene
Publisher :
Page : 740 pages
File Size : 30,9 MB
Release : 1951
Category : Equations of motion
ISBN :
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assumptions. Calculations of loads for different static longitudinal stability on two German airplane models, HC 45 and HS 122, are compared with flight tests. Good agreement is obtained between the trend of the flight tests and the calculated values; however no absolute comparison was possible between the flight tests and calculations.
Author : Y C Fung
Publisher : Courier Dover Publications
Page : 516 pages
File Size : 15,60 MB
Release : 2008-10-17
Category : Technology & Engineering
ISBN : 0486469360
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
Author : John C. Houbolt
Publisher :
Page : 94 pages
File Size : 33,83 MB
Release : 1950
Category : Aerodynamic load
ISBN :
Through the use of difference equations and matrix notation a systematic procedure is developed for the calculation of the structural response of an aircraft flying through a gust. The method takes into account wing bending and twisting flexibilities, fuselage flexibility, vertical and pitching motion of the airplane, and some tail forces. Strip theory is used, but approximate three-dimensional and compressibility corrections can be made without difficulty. Either sharp-edge or arbitrary gusts may be treated.
Author :
Publisher :
Page : 1168 pages
File Size : 25,72 MB
Release : 1912
Category : Aeronautics
ISBN :
Author : Louis V. Schmidt
Publisher : AIAA
Page : 426 pages
File Size : 20,41 MB
Release : 1998
Category : Aerodynamics
ISBN : 9781600860775