A Method for Obtaining the Nonlinear Aerodynamic Stability Characteristics of Bodies of Revolution from Free-flight Tests

A Method for Obtaining the Nonlinear Aerodynamic Stability Characteristics of Bodies of Revolution from Free-flight Tests PDF Author: Donn B. Kirk
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 52

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A Method for Obtaining the Nonlinear Aerodynamic Stability Characteristics of Bodies of Revolution from Free-Flight Tests

A Method for Obtaining the Nonlinear Aerodynamic Stability Characteristics of Bodies of Revolution from Free-Flight Tests PDF Author: Donn B. Kirk
Publisher: BiblioGov
ISBN: 9781289273897
Category :
Languages : en
Pages : 52

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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

A Method for Obtaining the Nonlinear Aerodynamic Stability Characteristics of Bodies of Revolution from Free-flight Tests PDF Author: Donn B. Kirk
Publisher:
ISBN:
Category :
Languages : en
Pages : 47

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NASA Technical Note

NASA Technical Note PDF Author:
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ISBN:
Category :
Languages : en
Pages : 446

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NASA Technical Report

NASA Technical Report PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 550

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Aerodynamic Testing in a Free-flight Spark Range

Aerodynamic Testing in a Free-flight Spark Range PDF Author: G. L. Winchenbach
Publisher:
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Category : Aerodynamics
Languages : en
Pages : 172

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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

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 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1746

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A Study of Damping in Nonlinear Oscillations

A Study of Damping in Nonlinear Oscillations PDF Author: Maurice L. Rasmussen
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Category : Damping (Mechanics)
Languages : en
Pages : 60

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Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448

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