Framework for establishing the limits of tabular aerodynamic models for flight dynamics analysis
Framework for establishing the limits of tabular aerodynamic models for flight dynamics analysis
978-1-60086-978-5
Ghoreyshi, M.
e43d6179-9d81-4c53-9057-9c7f8ec588fb
Badcock, K. J.
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Da Ronch, A.
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Swift, A.
9897ec7a-5a18-43f5-9da9-8e6141b5d60a
Marques, S.
5ea29e28-64ed-487f-9274-eeb5f57d03be
Ames, N.
8f30dcef-18aa-4555-abc4-e74c3c3d39ef
August 2009
Ghoreyshi, M.
e43d6179-9d81-4c53-9057-9c7f8ec588fb
Badcock, K. J.
64c4dc5d-1f2f-4358-af31-f6506c1810ef
Da Ronch, A.
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Swift, A.
9897ec7a-5a18-43f5-9da9-8e6141b5d60a
Marques, S.
5ea29e28-64ed-487f-9274-eeb5f57d03be
Ames, N.
8f30dcef-18aa-4555-abc4-e74c3c3d39ef
Ghoreyshi, M., Badcock, K. J., Da Ronch, A., Swift, A., Marques, S. and Ames, N.
(2009)
Framework for establishing the limits of tabular aerodynamic models for flight dynamics analysis.
AIAA Guidance, Navigation, and Control Conference, Chicago, United States.
10 - 13 Aug 2009.
(doi:10.2514/6.2009-6273).
Record type:
Conference or Workshop Item
(Paper)
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Published date: August 2009
Venue - Dates:
AIAA Guidance, Navigation, and Control Conference, Chicago, United States, 2009-08-10 - 2009-08-13
Organisations:
Aerodynamics & Flight Mechanics Group
Identifiers
Local EPrints ID: 353670
URI: http://eprints.soton.ac.uk/id/eprint/353670
ISBN: 978-1-60086-978-5
PURE UUID: ddc9f2f0-fa5e-43fd-907e-1c685e7c846f
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Date deposited: 13 Jun 2013 12:57
Last modified: 15 Mar 2024 03:46
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Contributors
Author:
M. Ghoreyshi
Author:
K. J. Badcock
Author:
A. Swift
Author:
S. Marques
Author:
N. Ames
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