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Shane Donovan
Institution:
Northrop Grumman (United States)
Observed institution:
Northrop Grumman (United States)
OpenAlex ID:
A5043149216
Effects of disciplinary uncertainty on multi-objective optimization in aircraft conceptual design
2011
·
Matthew J. Daskilewicz
, Brian J. German
, et al.
·
Structural and Multidisciplinary Optimization
·
36
A Systems Engineering Approach to the Application of Multidisciplinary Design, Analysis and Optimization (MDAO) for Efficient Supersonic Air-Vehicle Exploration (ESAVE)
2012
·
Wayne Hurwitz
, Shane Donovan
, et al.
·
AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference (MAO)
·
12
Form Factor and Critical Mach Number Estimation for Finite Wings
2012
·
Timothy J. Takahashi
, Brian J. German
, et al.
·
Journal of Aircraft
·
12
A Rapid Synthesis Method to Develop Conceptual Design Transonic Wing Lofts
2010
·
Shane Donovan
, Timothy Takahashi
·
AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference (MAO)
·
12
Non Planar Span Loads for Minimum Induced Drag
2011
·
Timothy Takahashi
, Shane Donovan
·
AIAA Aerospace Sciences Meeting
·
10
Enhanced Conceptual Wing Weight Estimation Through Structural Optimization and Simulation
2010
·
Jason Petermeier
, George Radtke
, et al.
·
AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference (MAO)
·
7
Zero Lift Drag and Drag Divergence Prediction for Finite Wings in Aircraft Conceptual Design
2010
·
Timothy Takahashi
, Brian German
, et al.
·
AIAA Aerospace Sciences Meeting
·
7
Wing Twist Design Considerations for Transport Category Aircraft
2011
·
Shane Donovan
, Timothy Takahashi
·
AIAA Aerospace Sciences Meeting
·
6
Optimum Transverse Span Loads for Transport Category Aircraft
2011
·
Shane Donovan
, Timothy Takahashi
, et al.
·
AIAA Aerospace Sciences Meeting
·
5
Weight Estimation for Composite Wings Based on Optimized Structure with Laminate Selection
2012
·
Matthew Stohr
, Jason Petermeier
, et al.
·
AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference (MAO)
·
2
Wing Section Thickness and Camber Allocation for Conceptual and Preliminary Aircraft Design
2011
·
Arvin Shajanian
, Timothy Takahashi
, et al.
·
AIAA Aerospace Sciences Meeting
·
2
Robust Design Considerations in the Multi-Objective Problem of Aircraft Conceptual Design
2010
·
Matthew Daskilewicz
, Brian German
, et al.
·
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM)
·
2
Zero Lift Drag and Drag Divergence Prediction for Finite Wings in Aircraft Design
2010
·
Timothy T. Takahashi
, Northrop Grumman
, et al.
·
2
Incorporation of Mission Payload Power and Thermal Requirements into the Multi-Disciplinary Aircraft Performance and Sizing Process
2010
·
Timothy Takahashi
, Shane Donovan
·
AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference (MAO)
·
1
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Works count:
14
Citation count:
116
H-index:
7
I10-index:
5
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