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Lloyd B Eldred
Lloyd B Eldred
Vehicle Analysis Branch, Langley Research Center, NASA
Bestätigte E-Mail-Adresse bei nasa.gov
Titel
Zitiert von
Zitiert von
Jahr
Kelvin-Voigt versus fractional derivative model as constitutive relations for viscoelastic materials
LB Eldred, WP Baker, AN Palazotto
AIAA journal 33 (3), 547-550, 1995
1861995
Numerical application of fractional derivative model constitutive relations for viscoelastic materials
LB Eldred, WP Baker, AN Palazotto
Computers & structures 60 (6), 875-882, 1996
501996
Viscoelastic material response with a fractional-derivative constitutive model
WP Baker, LB Eldred, AN Palazotto
AIAA journal 34 (3), 596-600, 1996
181996
Sensitivity analysis of a wing aeroelastic response
RK Kapania, LB Eldred, JFM Barthelemy
Journal of aircraft 30 (4), 496-504, 1993
101993
Structural analysis in a conceptual design framework
S Padula, J Robinson, L Eldred
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2012
82012
Structural Weight Estimation for Launch Vehicles
J Cerro, Z Martinovic, P Su, L Eldred
61st International Conference on Mass Properties Engineering, 2002
82002
Sensitivity analysis of aeroelastic response of a wing using piecewise pressure representation
LB Eldred, RK Kapania, JFM Barthelemy
Journal of aircraft 33 (4), 803-807, 1996
81996
Integration of high fidelity structural analysis into parallel multidisciplinary aircraft analysis
L Eldred, C Byun, G Guruswamy
39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 1998
71998
Loft: An Automated Mesh Generator for Stiffened-Shell Aerospace Vehicles
LB Eldred
52023
Enabling Rapid and Robust Structural Analysis During Conceptual Design
LB Eldred, SL Padula, W Li
National Aeronautics and Space Administration, Langley Research Center, 2015
52015
Reference Models for Structural Technology Assessment and Weight Estimation
J Cerro, Z Martinovic, L Eldred
SAWE 64th International Conference on Mass Properties Engineering, 2005
32005
User's Guide for ENSAERO_FE Parallel Finite Element Solver
LB Eldred, GP Guruswamy
31999
Sensitivity analysis of the static aeroelastic response of a wing
LB Eldred
Virginia Tech, 1993
31993
Application of fractional derivative model constitutive relations for viscoelastic materials
L Eldred, W Baker, A Palazotto
36th Structures, Structural Dynamics and Materials Conference, 1426, 1995
21995
Advanced Composites Project Overview: Advanced Air Vehicles Program
LB Eldred
TCC (The Composites Consortium) Fall 2015 Technical Meeting, 2015
12015
Solution of non-linear partial differential equations with the Chebyshev Spectral method
LB Eldred
Virginia Tech, 1989
11989
Loft, An Automated Parametric Mesh Generator for Stiffened Shell Aerospace Vehicles
LB Eldred
AIAA SCITECH 2024 Forum, 2459, 2024
2024
Two Decades of Aerospace Vehicle Analysis with HyperSizer and HyperX
LB Eldred
HyperX Users Conference, 2023
2023
Advanced Composite Structures At NASA Langley Research Center
LB Eldred
International Conference on Emerging Trends in Technology and Applied Sciences, 2015
2015
SITPS Analysis and Sizing on RALV Orbiter
K Bey, L Eldred, K Martin
NASA Fundamental Aeronautics Program Technical Conference 2011, 2011
2011
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