Author: Donn B. Kirk
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 52
Book Description
A Method for Obtaining the Nonlinear Aerodynamic Stability Characteristics of Bodies of Revolution from Free-flight Tests
Author: Donn B. Kirk
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 52
Book Description
A Method for Obtaining the Nonlinear Aerodynamic Stability Characteristics of Bodies of Revolution from Free-Flight Tests
Author: Donn B. Kirk
Publisher: BiblioGov
ISBN: 9781289273897
Category :
Languages : en
Pages : 52
Book Description
A method is presented for obtaining the nonlinear aerodynamic stability characteristics of bodies of revolution from free-flight test.s The necessary conditions for the application of this method are: (1) that the roll rate and damping encountered in a single cycle of oscillation be small, and (2) that the resulting motion be reasonably planar. Four approximations to the nonlinear restoring moment are considered and solutions are obtained in closed form: 1. A single-term polynomial in an arbitrary power of the angle of attack. 2. A two-term polynomial having linear and cubic terms. 3. A three-term polynomial having linear, quadratic, and cubic terms. 4. A three-term polynomial having linear, quadratic, and cubic terms. An iteration procedure is formulated to allow the use of each of these approximations for obtaining the aerodynamic coefficients of bodies of revolution from free-flight test data. It is found that although the equations that are solved pertain strictly to planar motion, the solutions are applicable to motions that deviate to a fairly large degree from planar motion.
Publisher: BiblioGov
ISBN: 9781289273897
Category :
Languages : en
Pages : 52
Book Description
A method is presented for obtaining the nonlinear aerodynamic stability characteristics of bodies of revolution from free-flight test.s The necessary conditions for the application of this method are: (1) that the roll rate and damping encountered in a single cycle of oscillation be small, and (2) that the resulting motion be reasonably planar. Four approximations to the nonlinear restoring moment are considered and solutions are obtained in closed form: 1. A single-term polynomial in an arbitrary power of the angle of attack. 2. A two-term polynomial having linear and cubic terms. 3. A three-term polynomial having linear, quadratic, and cubic terms. 4. A three-term polynomial having linear, quadratic, and cubic terms. An iteration procedure is formulated to allow the use of each of these approximations for obtaining the aerodynamic coefficients of bodies of revolution from free-flight test data. It is found that although the equations that are solved pertain strictly to planar motion, the solutions are applicable to motions that deviate to a fairly large degree from planar motion.
A Method for Obtaining the Nonlinear Aerodynamic Stability Characteristics of Bodies of Revolution from Free-flight Tests
Author: Donn B. Kirk
Publisher:
ISBN:
Category :
Languages : en
Pages : 47
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 47
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 446
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 446
Book Description
NASA Technical Report
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 550
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 550
Book Description
Aerodynamic Testing in a Free-flight Spark Range
Author: G. L. Winchenbach
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 172
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 172
Book Description
Free-flight Investigation of the Static Stability and Aerodynamic Drag of Three Blunt- Nosed Cylinder-flare Test Bodies at Mach Numbers from 13 to 17
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1746
Book Description
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1746
Book Description
A Study of Damping in Nonlinear Oscillations
Author: Maurice L. Rasmussen
Publisher:
ISBN:
Category : Damping (Mechanics)
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category : Damping (Mechanics)
Languages : en
Pages : 60
Book Description
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description