41 Publications (Page 2 of 2)
1989
Zeiler, T.A. Pototzky, A.S., "On the Relationship Between Matched Filter Theory as Applied to Gust Loads and Phased Design Loads Analysis," NASA CR - 181802, April, 1989
Zeiler, Thomas A
1989
1988
Dynamic analysis of an unrestrained, rotating structure through nonlinear simulation
Zeiler, Thomas A and Buttrill, Carey S
Structures, Structural Dynamics and Materials Conference, 29th, Williamsburg, VA, Technical Papers. Part 1; 18-20 Apr. 1988. 1988. | Conference Proceeding
 
Zeiler, T. A. and Weisshaar, T. A., "Integrated Aeroservoelastic Tailoring of Lifting Surfaces," AIAA Journal of Aircraft, V.25, N.1, Jan. 1988, pp 76-83
Zeiler, Thomas A
1988
1987
A new simulation model building process for use in dynamic systems integration research
Arbuckle, P. D⋅Buttrill, Carey S and Zeiler, Thomas A
AIAA Flight Simulation Technologies Conference, Monterey, CA, Technical Papers; 17-19 Aug. 1987. 1987. | Conference Proceeding
 
Nonlinear simulation of a flexible aircraft in maneuvering flight
Buttrill, Carey S⋅Arbuckle, P. D and Zeiler, Thomas A
AIAA Flight Simulation Technologies Conference, Monterey, CA, Technical Papers; 17-19 Aug. 1987. 1987. | Conference Proceeding
1986
Integrated aeroservoelastic tailoring of lifting surfaces
Zeiler, Thomas A and WEISSHAAR, T. A
Structures, Structural Dynamics and Materials Conference, 27th, San Antonio, TX; UNITED STATES; 19-21 May 1986. 1986. | Conference Proceeding
1985
AN APPROACH TO INTEGRATED AEROSERVOELASTIC TAILORING FOR STABILITY (AEROELASTICITY, MULTIDISCIPLINARY DESIGN, STRUCTURAL OPTIMIZATION, UNSTEADY AERODYNAMICS) (Dissertation)
Zeiler, Thomas A (1985).
1983
Dynamic stability of flexible forward swept wing aircraft
WEISSHAAR, T. A and Zeiler, Thomas A
Journal of Aircraft (ISSN 0021-8669), vol. 20, pp. 1014-1020, 1983. | Journal Article
 
Dynamic stability of flexible forward swept wing aircraft
WEISSHAAR, T. A and Zeiler, Thomas A
Journal of Aircraft, vol. 20, 1983. | Journal Article
 
Dynamic stability of flexible forward swept wing aircraft.
Weisshaar, T. A and Zeiler, Thomas A
J. AIRCRAFT., vol. 20, (no. 12), pp. 1014-1020, 1983. | Journal Article
1982
Dynamic stability of flexible forward swept wing aircraft
WEISSHAAR, T. A and Zeiler, Thomas A
American Institute of Aeronautics and Astronautics, Atmospheric Flight Mechanics Conference, 9th, San Diego, CA; United States; 9-11 Aug. 1982. 1982. | Conference Proceeding
 
Dynamic stability of flexible forward swept wing aircraft.
Weisshaar, TA and Zeiler, Thomas A
AIAA, 1982. | Journal Article
 
Flutter of forward swept wings, analyses and tests
WEISSHAAR, T. A⋅Zeiler, Thomas A⋅HERTZ, T. J and SHIRK, M. H
Structures, Structural Dynamics and Materials Conference, 23rd, New Orleans, LA, Collection of Technical Papers, Part 2 ; United States; 10-12 May 1982. 1982. | Conference Proceeding
 
Flutter of Forward Swept Wings, Analyses and Tests.
Weisshaar, TA⋅Zeiler, Thomas A⋅Hertz, TJ and Shirk, MH
AM. INST. AERONAUT. & ASTRONAUT. (AIAA), 1982. | Journal Article
 
Flutter of Forward Swept Wings, Analyses and Tests.
Weisshaar, T. A⋅Zeiler, Thomas A⋅Hertz, T. J and Shirk, M. H
AM. INST. AERONAUT. & ASTRONAUT. (AIAA), 1290 AVE. AMERICAS, NEW YORK, NY 10104, 1982. 1982. | Conference Proceeding
n.d.no date or unknown
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. 1/2), pp. 176-90. | Journal Article