41 Publications (Page 1 of 2)
2006
Dynamics of Flexible Launch Vehicles with Variable Mass
Huang, Xiao and Zeiler, Thomas A
44th AIAA Aerospace Sciences Meeting and Exhibit; Reno, NV; USA; 9-12 Jan. 2006. 2006. | Conference Proceeding
2004
Determining worst-case gust loads on aircraft structures using an evolutionary algorithm
Karr, Charles LMehrotra, Rajiv and Zeiler, Thomas A
Applied Intelligence, vol. 20, (no. 2), pp. 135-145, 2004. | Journal Article
 
Determining Worst-Case Gust Loads on Aircraft Structures Using An Evolutionary Algorithm
Karr, C. L.Zeiler, Thomas A and Mehrotra, R.
(pp. 135 - 145). 2004
2002
Use of structural dynamic and fatigue sensitivity derivatives in an automotive design optimization
Zeiler, Thomas A
Structural and Multidisciplinary Optimization, vol. 23, (no. 5), pp. 390-397, 2002. | Journal Article
 
Use of Structural Dynamic and Fatigue Sensitivity Derivatives in An Automotive Design Optimization
Zeiler, Thomas A
(pp. 390 - 397). Jun 2002
2001
Design sensitivities of fatigue performance and structural dynamic response in an automotive application
Zeiler, Thomas A and Barkey, Mark E
Structural and Multidisciplinary Optimization, vol. 21, (no. 4), pp. 309-315, 2001. | Journal Article
 
Preliminary results of BE-1900D operational flight loads data evaluation
Zeiler, Thomas ATipps, Daniel OSkinn, Donald A and Rustenberg, John W
Journal of Aircraft (0021-8669), vol. 38, (no. 3), pp. 565-572, 2001. | Journal Article
2000
Analytical design sensitivity derivatives of time and frequency responses as an aid to the design process
Zeiler, Thomas A and Barkey, Mark E
International Journal of Vehicle Design, vol. 23, (no. 1), pp. 176-190, 2000. | Journal Article
 
Analytical design sensitivity derivatives of time and frequency responses as an aid to the design process
Zeiler, Thomas A and Barkey, Mark E
International Journal of Vehicle Design, 2000. | Journal Article
 
Analytical Design Sensitivity Derivatives of Time and Frequency Responses As An Aid to the Design Process
Zeiler, Thomas A and Barkey, M. E.
(pp. 176-190). Jan 2000
 
Genetic Algorithm for Optimizing the Gust Loads for Predicting Aircraft Aircraft Loads and Dynamic Response
Mehrotra, RajivKarr, C. and Zeiler, Thomas A
2000
 
Results of Theodorsen and Garrick revisited (error analysis of flutter boundaries in NACA reports)
Zeiler, Thomas A
Journal of Aircraft, vol. 37, (no. 5), pp. 918-920, 2000. | Journal Article
 
The Results of Theodorsen and Garrick Revisited
Zeiler, Thomas A
(pp. 918-920). Sep 2000
1999
Divergence and convergence of iterative static aeroelastic solutions
Zeiler, Thomas A
Journal of Aircraft (0021-8669), vol. 36, (no. 4), pp. 716-718, 1999. | Journal Article
 
Preliminary static aeroelastic analysis of reusable launch vehicle stability and control derivatives
Zeiler, Thomas AMcGhee, David and Brunty, Joseph A
Journal of Spacecraft and Rockets (USA), vol. 36, (no. 1), pp. 67-74, 1999. | Journal Article
 
Preliminary Static Aeroelastic Analysis of Stability and Control Derivatives of a Reusable Launch Vehicle
Zeiler, Thomas A
(pp. 67-74). Jan 1999
1998
Static aeroelastic considerations for circulation control airfoils
Zeiler, Thomas A
Journal of Aircraft (0021-8669), vol. 35, (no. 1), pp. 152-154, 1998. | Journal Article
1997
Matched filter concept and maximum gust loads
Zeiler, Thomas A
Journal of Aircraft, vol. 34, (no. 1), pp. 101-108, 1997. | Journal Article
1993
Aeroelastic character of a National Aerospace Plane demonstrator concept
Spain, Charles VZeiler, Thomas AGibbons, Michael DSoistmann, David LPozefsky, PeterDejesus, Rafael O and Brannon, Cyprian P
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 34th and AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Technical Papers. Pt. 1; 19-22 Apr. 1993. 1993. | Conference Proceeding
 
Aerothermoelastic analysis of a NASP demonstrator model
Heeg, JenniferZeiler, Thomas APototzky, Anthony SSpain, Charles V and Engelund, Walter C
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 34th and AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Technical Papers. Pt. 1; 19-22 Apr. 1993. 1993. | Conference Proceeding
 
Control/Structure Optimization By Multilevel Decomposition
Zeiler, Thomas A and Gilbert, M.G.
(pp. 99-107). 1993
 
Heeg, J., Zeiler, T.A., et al, "Aerothermoelastic Analysis of a NASP Demonstrator Model," AIAA SDM Conference, La Jolla, CA, Apr. 19-22, 1993
Zeiler, Thomas A
1993
 
Integrated control/structure optimization by multilevel decomposition
Zeiler, Thomas A and Gilbert, M. G
Structural and Multidisciplinary Optimization, vol. 6, (no. 2), pp. 99-107, 1993. | Journal Article
1991
Calculating Time-Correlated Gust Loads Using Matched Filter and Random Process Theories
Potozky, A.S.Zeiler, Thomas A and Perry, Boyd III
(pp. 346-352). May 1991
1989
Simulation Model Building Procedure for Dynamics Systems Integration
Buttrill, C. S.Arbuckle, P. D. and Zeiler, Thomas A
Nov 1989