Global Modeling of Pitch Damping from Flight Data-Reference-Cited by-同舟云学术

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Global Modeling of Pitch Damping from Flight Data

Published:2006-06-25 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
Short-container-title:

Author:

Favaregh Noah¹,Landman Drew¹

Affiliation:

1. Old Dominion University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6145

Reference15 articles.

1. 1DeLoach,R."TacticalDefensesAgainstSystematicVariationinWindTunnelTesting,"AIAApaper2002-0885.

2. 2DeLoach, R., and Berrier, BL. "Productivity and Quality Enhancements in a Configuration Aerodynamics Test using the Modern DesignofExperiments,"AIAApaper 2004-1145.

3. 3DeLoach,R."MDOEPerspectivesonWindTunnelTestingObjectives,"AIAApaper2002-2796.

4. 4Landman,D.,et.al."AHighPerformanceAircraftWindTunnelTestusingResponseSurfaceMethodologies,"AIAA paper 2005-7602.

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1. Global aircraft aero-propulsive linear parameter-varying model using design of experiments;Aerospace Science and Technology;2012-10

2. Forced Oscillation Wind Tunnel Testing for FASER Flight Research Aircraft;AIAA Atmospheric Flight Mechanics Conference;2012-08-13

3. Magnus and Spin-Damping Measurements of a Spinning Projectile Using Design of Experiments;Journal of Spacecraft and Rockets;2010-11

4. Stability Derivative Modeling Based on Aircraft Flight Modes Using Design of Experiments;15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2008-04-28

5. Development of a Low-Cost Sub-Scale Aircraft for Flight Research: The FASER Project;25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2006-06-05

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