41 Publications (Page 1 of 2)
2006
Dynamics of Flexible Launch Vehicles with Variable MassHuang, Xiao and Zeiler, Thomas A44th 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 algorithmKarr, Charles L⋅Mehrotra, Rajiv and Zeiler, Thomas AApplied Intelligence, vol. 20, (no. 2), pp. 135-145, 2004.
| Journal Article
Determining Worst-Case Gust Loads on Aircraft Structures Using An Evolutionary AlgorithmKarr, 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 optimizationZeiler, Thomas AStructural 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 OptimizationZeiler, Thomas A(pp. 390 - 397). Jun 2002
2001
Design sensitivities of fatigue performance and structural dynamic response in an automotive applicationZeiler, Thomas A and Barkey, Mark EStructural and Multidisciplinary Optimization, vol. 21, (no. 4), pp. 309-315, 2001.
| Journal Article
Preliminary results of BE-1900D operational flight loads data evaluationZeiler, Thomas A⋅Tipps, Daniel O⋅Skinn, Donald A and Rustenberg, John WJournal 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 processZeiler, Thomas A and Barkey, Mark EInternational 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 processZeiler, Thomas A and Barkey, Mark EInternational Journal of Vehicle Design, 2000.
| Journal Article
Analytical Design Sensitivity Derivatives of Time and Frequency Responses As An Aid to the Design ProcessZeiler, 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 ResponseMehrotra, Rajiv⋅Karr, C. and Zeiler, Thomas A2000
Results of Theodorsen and Garrick revisited (error analysis of flutter boundaries in NACA reports)Zeiler, Thomas AJournal of Aircraft, vol. 37, (no. 5), pp. 918-920, 2000.
| Journal Article
The Results of Theodorsen and Garrick RevisitedZeiler, Thomas A(pp. 918-920). Sep 2000
1999
Divergence and convergence of iterative static aeroelastic solutionsZeiler, Thomas AJournal 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 derivativesZeiler, Thomas A⋅McGhee, David and Brunty, Joseph AJournal 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 VehicleZeiler, Thomas A(pp. 67-74). Jan 1999
1998
Static aeroelastic considerations for circulation control airfoilsZeiler, Thomas AJournal of Aircraft (0021-8669), vol. 35, (no. 1), pp. 152-154, 1998.
| Journal Article
1997
Matched filter concept and maximum gust loadsZeiler, Thomas AJournal of Aircraft, vol. 34, (no. 1), pp. 101-108, 1997.
| Journal Article
1993
Aeroelastic character of a National Aerospace Plane demonstrator conceptSpain, Charles V⋅Zeiler, Thomas A⋅Gibbons, Michael D⋅Soistmann, David L⋅Pozefsky, Peter⋅Dejesus, Rafael O and Brannon, Cyprian PAIAA/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 modelHeeg, Jennifer⋅Zeiler, Thomas A⋅Pototzky, Anthony S⋅Spain, Charles V and Engelund, Walter CAIAA/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 DecompositionZeiler, 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, 1993Zeiler, Thomas A1993
Integrated control/structure optimization by multilevel decompositionZeiler, Thomas A and Gilbert, M. GStructural 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 TheoriesPotozky, A.S.⋅Zeiler, Thomas A and Perry, Boyd III(pp. 346-352). May 1991
1989
Simulation Model Building Procedure for Dynamics Systems IntegrationButtrill, C. S.⋅Arbuckle, P. D. and Zeiler, Thomas ANov 1989