Author: S. L. WalkdenPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 278
Book Description
Aeroplanes in Gusts
Author: S. L. WalkdenPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 278
Book Description
Aeroplanes in Gusts
Author: S. L. WalkdenPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 280
Book Description
Gust Loads on Aircraft
Author: Frederic M. HoblitPublisher: AIAA
ISBN: 9781600860607
Category : Airplanes
Languages : en
Pages : 332
Book Description
How to Understand Aeroplanes
Author: S. L. WalkdenPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 138
Book Description
Structural Response to Discrete and Continuous Gusts of an Airplane Having Wing-bending Flexibility and a Correlation of Calculated and Flight Results
Author: Antonio FerriPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 278
Book Description
Influence of Static Longitudinal Stability on the Behavior of Airplanes in Gusts
Author: H. HoenePublisher:
ISBN:
Category : Equations of motion
Languages : en
Pages : 740
Book Description
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.
An Introduction to the Theory of Aeroelasticity
Author: Y C FungPublisher: Courier Dover Publications
ISBN: 0486469360
Category : Technology & Engineering
Languages : en
Pages : 516
Book Description
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
A Recurrence Matrix Solution for the Dynamic Response of Aircraft in Gusts
Author: John C. HouboltPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 94
Book Description
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.
The Mastery of the Air
Author: William J. ClaxtonPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 290
Book Description
Author: Alexander Klemin