An Evaluation of an Analytical Technique for the Prediction of the Spin and Spin Recovery Characteristics of a Contemporary Airplane PDF Download
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Author: R. H. HANNA
Publisher:
ISBN:
Category :
Languages : en
Pages : 173
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Book Description
THE EVALUATION OF AN ANALYTICAL METHOD FOR THE PREDICTION OF SPIN AND SPIN RECOVERY CHARACTERISTICS OF A CONTEMPORARY AIRPLANE IS DESCRIBED. The spin characteristics of an airplane can be accurately determined through the use of static wind tunnel data and estimated rotary and damping derivations based on static wind tunnel data. (Author).
Author: R. H. HANNA
Publisher:
ISBN:
Category :
Languages : en
Pages : 173
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Book Description
THE EVALUATION OF AN ANALYTICAL METHOD FOR THE PREDICTION OF SPIN AND SPIN RECOVERY CHARACTERISTICS OF A CONTEMPORARY AIRPLANE IS DESCRIBED. The spin characteristics of an airplane can be accurately determined through the use of static wind tunnel data and estimated rotary and damping derivations based on static wind tunnel data. (Author).
Author: William D. Grantham
Publisher:
ISBN:
Category : Spin (Aerodynamics)
Languages : en
Pages : 52
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 152
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Book Description
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 464
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Book Description
Author: William D. Grantham
Publisher:
ISBN:
Category : Spin (Aerodynamics)
Languages : en
Pages : 54
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Book Description
Author: James S. Bowman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Book Description
A summary was made of all NASA (and NACA) research and experience related to the spin and recovery characteristics of light personal-owner-type general-aviation airplanes. Very little of the research deals with light general-aviation airplanes as such, but many of the airplanes and models tested before and during World War II were similar to present-day light general-aviation airplanes with regard to the factors that are important in spinning. The material is based mainly on the results of spin-tunnel tests of free-spinning dynamically scaled models of about 100 different airplane designs and, whenever possible, includes correlation with full-scale spin tests. The research results are discussed in terms of airplane design considerations and the proper use of controls for recovery.
Author: William Mansfield Adams
Publisher:
ISBN:
Category : Equations of motion
Languages : en
Pages : 52
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Book Description
The nonlinear equations of motion are solved algebraically for conditions for which an airplane is in an equilibrium spin. Constrained minimization techniques are employed in obtaining the solution. Linear characteristics of the airplane about the equilibrium points are also presented and their significance in identifying the stability characteristics of the equilibrium points is discussed. Computer time requirements are small making the method appear potentially applicable in airplane design. Results are obtained for several configurations and are compared with other analytic-numerical methods employed in spin prediction. Correlation with experimental results is discussed for one configuration for which a rather extensive data base was available. A need is indicated for higher Reynolds number data taken under conditions which more accurately simulate a spin.
Author: Ernie L. Anglin
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 96
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Author: Carlton William Carroll
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
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Book Description
Author: Ernie L. Anglin
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 60
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Book Description
