Crossref Citations
This Book has been
cited by the following publications. This list is generated based on data provided by Crossref.
Livne, Eli
2003.
Future of Airplane Aeroelasticity.
Journal of Aircraft,
Vol. 40,
Issue. 6,
p.
1066.
Sadr Lahidjani, M. H.
Haddadpour, Hassan
and
Shams, Shahrokh
2004.
Nonlinear Aeroelastic Behavior of a High Flexibility Wing with Long Span Considering Large Deflection.
Patil, Mayuresh J.
Yurkovich, Rudolph N.
and
Hodges, Dewey H.
2004.
Incorrectness of the k Method for Flutter Calculations.
Journal of Aircraft,
Vol. 41,
Issue. 2,
p.
402.
Pettit, Chris
2004.
Engineering Design Reliability Handbook.
Traub, Lance W.
Miller, Adam
and
Rediniotis, Othon
2004.
Effects of Active and Passive Flow Control on Dynamic-Stall Vortex Formation.
Journal of Aircraft,
Vol. 41,
Issue. 2,
p.
405.
Haddadpour, Hassan
Shams, Shahrokh
and
Kheiri, Mojtaba
2005.
Sharp Edge Gust Effects on Aeroelastic Behavior of a Flexible Wing with High Aspect Ratio.
Teng, Ying
and
Chen, Hsin-Piao
2005.
Analysis of Active Flutter Suppression with Leading- and Trailing-Edge Control Surfaces via μ-Method.
Vol. 1,
Issue. ,
RUBILLO, CHRISTINA
MARZOCCA, PIERGIOVANNI
and
BOLLT, ERIK
2006.
ACTIVE AEROELASTIC CONTROL OF LIFTING SURFACES VIA JET REACTION LIMITER CONTROL.
International Journal of Bifurcation and Chaos,
Vol. 16,
Issue. 09,
p.
2559.
Sapdoni, Alessandro
and
Ruzzene, Massimo
2006.
Numerical and Experimental Analysis of the Static and Dynamic Morphing Characteristics of a Chiral Core Airfoil.
p.
419.
Teng, Ying
and
Chen, Hsin-Piao
2006.
u-Synthesis for An Active Aeroelastic Wing with Leading and Trailing Edge Control Surfaces.
Buckholtz, Kenneth R.
Wise, Kevin A.
and
Ferman, Marty A.
2007.
Static Feedback Control Augmented with an Adaptive Neural Network Applied to an Aerospace Structure.
p.
3919.
Spadoni, Alessandro
and
Ruzzene, Massimo
2007.
Numerical and experimental analysis of the static compliance of chiral truss-core airfoils.
Journal of Mechanics of Materials and Structures,
Vol. 2,
Issue. 5,
p.
965.
Hodges, Dewey H.
Saberi, Hossein
and
Ormiston, Robert A.
2007.
Development of Nonlinear Beam Elements for Rotorcraft Comprehensive Analyses.
Journal of the American Helicopter Society,
Vol. 52,
Issue. 1,
p.
36.
Hodges, Dewey H.
2007.
Bending-Torsion Divergence of a Clamped-Clamped Composite Wing.
Journal of Aircraft,
Vol. 44,
Issue. 6,
p.
2070.
Pitt, Dale
2007.
A Novel Technique for Educating Aeroelasticity Engineers.
Wickert, Douglas
and
Canfield, Robert
2008.
Least-Squares Continuous Sensitivity Analysis of an Example Fluid-Structure Interaction Problem.
Trikha, Manish
Roy Mahapatra, Debiprosad
Gopalakrishnan, S.
and
Pandiyan, R.
2008.
Analysis of Aeroelastic Stability of a Slender Launch Vehicle Using Aerodynamic Data.
Razi, M
and
Ghadiri, B
2008.
Aeroelastic response of a swept wing with cubic structural non-linearities.
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,
Vol. 222,
Issue. 2,
p.
229.
Bond, Vanessa
Canfield, Robert
Suleman, Afzal
and
Blair, Maxwell
2008.
Aeroelastic Scaling for Verification and Evaluation of Geometric Nonlinearity on a Joined-Wing Aircraft Model.
Attaran, A.
Majid, D. L.
Basri, Shahnor
Mohd Rafie, A. S.
and
Abdullah, E. J.
2008.
Structural optimization of an aeroelastically tailored composite flat plate made of woven fiberglass/epoxy.
Acta Mechanica,
Vol. 196,
Issue. 3-4,
p.
161.