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Coupling Dynamics in Aircraft: A Historical Perspective. NASA Special Publication SP-532, Research Engineering, NASA Dryden Flight Research Center

Day, Richard E. (1997) Coupling Dynamics in Aircraft: A Historical Perspective. NASA Special Publication SP-532, Research Engineering, NASA Dryden Flight Research Center. National Aeronautics and Space Administration.

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Abstract

Coupling dynamics can produce either adverse or beneficial stability and controllability, depending on the characteristics of the aircraft. This report presents archival anecdotes and analyses of coupling problems experienced by the X-series, Century series, and Space Shuttle aircraft. The three catastrophic sequential coupling modes of the X-2 airplane and the two simultaneous unstable modes of the X-15 and Space Shuttle aircraft are discussed. In addition, the most complex of the coupling interactions, inertia roll coupling, is discussed for the X-2, X-3, F-100A, and YF-102 aircraft. The mechanics of gyroscopics, centrifugal effect, and resonance in coupling dynamics are described. The coupling modes discussed are interacting multiple degrees of freedom of inertial and aerodynamic forces and moments. The aircraft are assumed to be rigid bodies. Structural couplings are not addressed. Various solutions for coupling instabilities are discussed.

EPrint Type:NASA Special Publication
Keywords:Coupling dynamics, Coupling modes, F-100 aircraft, Space Shuttle, X-2 aircraft, X-3 aircraft, X-15 aircraft, YF-102 aircraft
Subjects:Aircraft/Project: X-3
Aircraft/Project: F-100
(01 - 09) Aeronautics: (08) Aircraft Stability And Control
Aircraft/Project: YF-102
Aircraft/Project: X-15
Aircraft/Project: Space Shuttle Orbiter
Aircraft/Project: X-2
ID Code:169
Deposited On:14 June 2004
Additional Information:70 pages. Richard E. Day (NASA retired). Prepared under NASA contract NASA 2-13445, subcontract no. TSD-93-RED-2805.
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Last Modified: September 14, 2004
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