university of florida thesis or dissertation formatting template
university of florida thesis or dissertation formatting template
university of florida thesis or dissertation formatting template
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67. Cunningham, A. M., Jr., and den Boer, R. G., “Transonic Wind Tunnel Investigation <strong>of</strong><br />
Limit Cycle Oscillations on Fighter Type Wings - Update,” AIAA Paper 1992-2125,<br />
April 1992.<br />
68. Cunningham, A. M., Jr., “General Wind Tunnel Test Rep<strong>or</strong>t f<strong>or</strong> Limit Cycle Oscillation<br />
Test,” General Dynamics, Rep<strong>or</strong>t 16PR10965, June 1992.<br />
69. Cunningham, A. M., Jr., “Final Rep<strong>or</strong>t f<strong>or</strong> F-16 Limit Cycle Oscillation Investigation:<br />
Volume III – A Semi-Empirical Method f<strong>or</strong> Predicting Transonic Limit Cycle Oscillation<br />
Characteristics <strong>of</strong> Fighter Aircraft, Part 2 – Pressure Time Hist<strong>or</strong>y Analysis and<br />
Development <strong>of</strong> the LFWC Unsteady Aerodynamic Model f<strong>or</strong> LCO,” Lockheed F<strong>or</strong>t<br />
W<strong>or</strong>th Company, Rep<strong>or</strong>t 16PR11861, June 1994.<br />
70. Cunningham, A. M., Jr., and den Boer, R. G., “Overview <strong>of</strong> Unsteady Transonic Wind<br />
Tunnel Test on a Semispan Straked Delta Wing Oscillating in Pitch,” Wright Lab<strong>or</strong>at<strong>or</strong>y,<br />
Rep<strong>or</strong>t WL-TR-94-3017, August 1994.<br />
71. Cunningham, A. M., Jr., “A Generic Nonlinear Aeroelastic Method with Semi-empirical<br />
Nonlinear Unsteady Aerodynamics - Volume 1: Technical Discussion,” Air F<strong>or</strong>ce<br />
Research Lab<strong>or</strong>at<strong>or</strong>y, Rep<strong>or</strong>t AFRL-VA-WP-TR-1999-3014, February 1999.<br />
72. Cunningham, A. M., Jr., “The Role <strong>of</strong> Non-linear Aerodynamics in Fluid-Structure<br />
Interaction,” AIAA Paper 1998-2423, June 1998.<br />
73. Meijer, J. J., and Cunningham, A. M., Jr., “Understanding and Development <strong>of</strong> a<br />
Prediction Method <strong>of</strong> Transonic Limit Cycle Oscillation Characteristics <strong>of</strong> Fighter<br />
Aircraft,” AIAA Paper 1992-4501, 1992.<br />
74. Cunningham, A. M., Jr., and Meijer, J. J., “Semi-Empirical Unsteady Aerodynamics f<strong>or</strong><br />
Modeling Aircraft Limit Cycle Oscillations and Other Non-Linear Aeroelastic<br />
Problems,” Proceedings <strong>of</strong> the International F<strong>or</strong>um on Aeroelasticity and Structural<br />
Dynamics, Royal Aeronautical Society, London, Vol. 2, 1995, pp. 74.1-74.14.<br />
75. Meijer, J. J., and Cunningham, A. M., Jr., “A Semi-Empirical Unsteady Nonlinear<br />
Aerodynamic Model to Predict Transonic LCO Characteristics <strong>of</strong> Fighter Aircraft,”<br />
AIAA Paper 1995-1340, April 1995.<br />
76. Cunningham, A. M., Jr., “Aerodynamic Aspects <strong>of</strong> Transonic Limit Cycle Oscillations,”<br />
1994 Proceedings <strong>of</strong> the Aeroelasticity and Fluid Structure Interaction Problems,<br />
American Society <strong>of</strong> Mechanical Engineers, Chicago, Vol. 44, 1994, pp. 29-47.<br />
77. Melville, R., “Nonlinear Simulation <strong>of</strong> F-16 Aeroelastic Instability,” AIAA Paper 2001-<br />
0570, January 2001.<br />
78. Melville, R., “Nonlinear Mechanisms <strong>of</strong> Aeroelastic Instability f<strong>or</strong> the F-16,” AIAA<br />
Paper 2002-0817, January 2002.<br />
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