Estimating aircraft stability derivatives through finite element analysis

Collection of Technical Papers - AIAA Atmospheric Flight Mechanics Conference

Volumn 2, Issue , 2004, Pages 1023-1034

  Babcock, Deric A ^a,b   Arena Jr , Andrew S ^a,b  

^a OKLAHOMA STATE UNIVERSITY   (United States)

^b Mechanical and Aerospace Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT STABILITY; SLIP ANGLE; WING CHORD; WING SPAN;

AEROSPACE INDUSTRY; AIRCRAFT MODELS; BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; FINITE ELEMENT METHOD; FLOW PATTERNS; TRANSONIC FLOW; TRANSPIRATION; VELOCITY CONTROL;

AEROSPACE VEHICLES;

EID: 19644385643     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. USAF Stability and Control DATCOM, Flight Control Division, Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, Fairborn, OH.
2. Gupta, K. K., "STARS - An Integrated, Multidisciplinary, Finite-Element, Structural, Fluids, Aeroelastic, and Aeroservoelastic Analysis Computer Program," NASA TM-4795, April 2001.
3. Cowan, T. J., "Finite Element CFD Analysis of Super-Maneuvering and Spinning Structures," Ph.D. Dissertation, Mechanical and Aerospace Engineering Dept., Oklahoma State Univ., 2003.
4. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural dynamics, and Materials Conference, April, 1998 Long Beach, CA.
5. Boeckman, A. A., "Accelerating CFD-Based Aeroelastic Analysis Using Distributed Processing," Master's Thesis, Mechanical and Aerospace Engineering Dept., Oklahoma State Univ., 2003.
6. O'Neill, C. R., "Improved System Identification for Aeroservoelastic Predictions," Master's Thesis, Mechanical and Aerospace Engineering Dept., Oklahoma State Univ., 2003.
7. Klein, V., and Murphy P. C., "Aerodynamic Parameters of High Performance Aircraft Estimated from Wind Tunnel and Flight Test Data," AGARD Symposium on System Identification for Integrated Aircraft Development and Flight Testing, May, 1998, Madrid, Spain.
8. Klein, V., Murphy P. C., Curry, T. J., and Brandon, J. M., "Analysis of Wind Tunnel Longitudinal Static and Oscillatory Data of the F-16XL Aircraft," NASA TM-97-206276, December 1997.
9. Iliff, K. W., and Maine R. E., "Practical Aspects of Using a Maximum Likelihood Estimation Method to Extract Stability and Control Derivatives from Flight Data," NASA TN D-8209, April 1976.
10. nd Ed. McGraw-Hill, Boston, 1998.
11. Park, M. A., Green, L. L., Montgomer, R. C., and Raney, D. L., "Determination of Stability and Control Derivatives Using Computational Fluid Dynamics and Automatic Differentiation," AIAA 99-3136, June 1999.
12. Moes, T. R., Noffz, G. K., and Iliff K. W., "Results From F-18B Stability and Control Parameter Estimation Flight Tests at High Dynamic Pressures," NASA TP-2000-209033, November 2000.