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Edmund Pendleton
Observed names:
EDMUND PENDLETON,
Edmund W. Pendleton
Institution:
United States Air Force Research Laboratory
Observed institutions:
United States Air Force Research Laboratory,
Wright-Patterson Air Force Base,
United States Air Force,
Wright Laboratory,
Wright Research and Development Center
OpenAlex ID:
A5087491657
Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development
2000
·
Edmund W. Pendleton
, Denis Bessette
, et al.
·
Journal of Aircraft
·
239
Design and application of compliant mechanisms for morphing aircraft structures
2003
·
Sridhar Kota
, Joel A. Hetrick
, et al.
·
Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE
·
175
Application of Active Flexible Wing technology to the Agile Falcon
1992
·
Edmund Pendleton
, Mark Lee
, et al.
·
Journal of Aircraft
·
32
A Design Study Employing Aeroelastic Tailoring and an Active Aeroelastic Wing Design Approach on a Tailless Lambda Wing Configuration
2014
·
Edward J. Alyanak
, Edmund Pendleton
·
AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference (MAO)
·
17
Transonic aeroelastic models of highly swept hypersonic lifting surfaces
1995
·
Edmund Pendleton
, Greg Moster
, et al.
·
Journal of Aircraft
·
10
An Integrated Airframe Experiment for Future Responsive Access to Space Applications
2009
·
Robert Biggs
, Edmund Pendleton
, et al.
·
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM)
·
8
A Hybrid Launch Vehicle Design Concept Based on Recent Industry Studies --A Consensus View--
2008
·
Kenneth Griffin
, Edmund Pendleton
·
AIAA Aerospace Sciences Meeting and Exhibit
·
8
Integrated Composite Structures Demonstration for Future Space Launch Vehicle Airframe Applications
2012
·
Edmund Pendleton
, Robert Biggs
, et al.
·
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM)
·
4
Structural Efficiency of Integrated Composite Structures for Future Space Launch Vehicle Airframe Applications
2011
·
Robert Biggs
, Mark McCandless
, et al.
·
AIAA SPACE Conference & Exposition
·
3
An application of the active flexible wing concept to an F-16 derivative wing model
1991
·
EDMUND PENDLETON
, MARK LEE
, et al.
·
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM)
·
2
Ground Vibration Testing of Future responsive Access to Space Airframe Ground Experiment
2013
·
Paul Scott Zink
, Ben Clark
, et al.
·
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM)
·
1
A comparison of flutter analyses for a 45 deg swept model
1987
·
EDMUND PENDLETON
, MARK FRENCH
, et al.
·
AIAA Aircraft Design, Systems and Operations Meeting
·
1
Application of Active Flexible Wing Technology to the
1992
·
Edmund Pendleton
, Mark Lee
, et al.
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Works count:
13
Citation count:
500
H-index:
7
I10-index:
5
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