Author: S. L. Walkden
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 278
Book Description
Aeroplanes in Gusts
Author: S. L. Walkden
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 278
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 278
Book Description
Aeroplanes in Gusts
Author: S. L. Walkden
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 278
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 278
Book Description
How to Understand Aeroplanes
Author: S. L. Walkden
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 138
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 138
Book Description
Gust Loads on Aircraft
Author: Frederic M. Hoblit
Publisher: AIAA
ISBN: 9781600860607
Category : Airplanes
Languages : en
Pages : 332
Book Description
Publisher: AIAA
ISBN: 9781600860607
Category : Airplanes
Languages : en
Pages : 332
Book Description
An Introduction to the Theory of Aeroelasticity
Author: Y C Fung
Publisher: 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.
Publisher: 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.
Influence of Static Longitudinal Stability on the Behavior of Airplanes in Gusts
Author: H. Hoene
Publisher:
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.
Publisher:
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.
United States Naval Institute Proceedings
Author: United States Naval Institute
Publisher:
ISBN:
Category : Marine engineering
Languages : en
Pages : 2302
Book Description
Publisher:
ISBN:
Category : Marine engineering
Languages : en
Pages : 2302
Book Description
United States Naval Institute Proceedings
Author:
Publisher:
ISBN:
Category : Naval art and science
Languages : en
Pages : 1250
Book Description
Publisher:
ISBN:
Category : Naval art and science
Languages : en
Pages : 1250
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1078
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1078
Book Description