Verification of H Flutter AnalysisHOUNJET, Michaël H. L.Journal of aircraft. 2010, Vol 47, Num 6, pp 2168-2174, issn 0021-8669, 7 p.Article

H Flutter Analysis : A Direct Harmonic Interpolation MethodHOUNJET, Michaël H. L.Journal of aircraft. 2009, Vol 46, Num 1, pp 348-352, issn 0021-8669, 5 p.Article

Extension of flutter prediction parameter for multimode flutter systemsBAE, Jae-Sung; KIM, Jong-Yun; LEE, In et al.Journal of aircraft. 2005, Vol 42, Num 1, pp 285-288, issn 0021-8669, 4 p.Article

Upper-bound flutter speed estimation using the μ-k methodBORGLUND, Dan.Journal of aircraft. 2005, Vol 42, Num 2, pp 555-557, issn 0021-8669, 3 p.Article

Application of Pattern Search in Worst-Case Flutter SolutionYINGSONG GU; ZHICHUN YANG.Journal of aircraft. 2012, Vol 49, Num 6, pp 2089-2092, issn 0021-8669, 4 p.Article

Extension of the g-method flutter solution to aeroservoelastic stability analysisKARPEL, M; MOULIN, B; CHEN, P. C et al.Journal of aircraft. 2005, Vol 42, Num 3, pp 789-792, issn 0021-8669, 4 p.Article

Flutter Analysis: Using Piecewise Quadratic Interpolation with Mode Tracking and Wind-Tunnel TestsHUANG, R; QIAN, W. M; ZHAO, Y. H et al.Journal of aircraft. 2010, Vol 47, Num 4, pp 1447-1451, issn 0021-8669, 5 p.Article

Reduced-Order-Model-Based Flutter Analysis at High Angle of AttackWEIWEI ZHANG; ZHENGYIN YE.Journal of aircraft. 2007, Vol 44, Num 6, pp 2086-2089, issn 0021-8669, 4 p.Article

Supersonic Flutter Analysis of Vehicles at Incidence Based on Local Piston TheoryXIAOMING SHI; GUOAN TANG; BINGYUAN YANG et al.Journal of aircraft. 2012, Vol 49, Num 1, pp 333-337, issn 0021-8669, 5 p.Article

Uncertainty Quantification in Flutter Analysis for an Airfoil with Preloaded Free PlayLI YI; YANG ZHICHUN.Journal of aircraft. 2010, Vol 47, Num 4, pp 1454-1457, issn 0021-8669, 4 p.Article

Aeroelastic Flutter Produces Hummingbird Feather SongsCLARK, Christopher J; ELIAS, Damian O; PRUM, Richard O et al.Science (Washington, D.C.). 2011, Vol 333, Num 6048, pp 1430-1433, issn 0036-8075, 4 p.Article

Aeroelastic Analysis of Rotors With Flexible Disks and Alternate Blade MistuningBLEEG, James M; YANG, Ming-Ta; ELEY, James A et al.Journal of turbomachinery. 2009, Vol 131, Num 1, issn 0889-504X, 011011.1-011011.9Article

Discrete conservation and coupling strategies in nonlinear aeroelasticityMASSJUNG, Ralf.Computer methods in applied mechanics and engineering. 2006, Vol 196, Num 1-3, pp 91-102, issn 0045-7825, 12 p.Article

Flutter of a cantilevered elastic and viscoelastic stripPOKAZEYEV, V. V.Journal of applied mathematics and mechanics. 2008, Vol 72, Num 4, pp 446-451, issn 0021-8928, 6 p.Article

Assessment of Uncertain External Store Aerodynamics Using μ-p Flutter AnalysisHEINZE, Sebastian; RINGERTZ, Ulf; BORGLUND, Dan et al.Journal of aircraft. 2009, Vol 46, Num 3, pp 1062-1068, issn 0021-8669, 7 p.Article

Robust Flutter Analysis Considering Mode Shape VariationsHEINZE, Sebastian; BORGLUND, Dan.Journal of aircraft. 2008, Vol 45, Num 3, pp 1070-1075, issn 0021-8669, 6 p.Article

A receptance-based method for predicting latent roots and critical points in friction-induced vibration problems of asymmetric systemsHUAJIANG OUYANG; BAEZA, Luis; SHAOLIN HU et al.Journal of sound and vibration. 2009, Vol 321, Num 3-5, pp 1058-1068, issn 0022-460X, 11 p.Article

Static and dynamic stabilities of a microbeam actuated by a piezoelectric voltageREZAZADEH, Ghader; FATHALILOU, Mohammad; SHABANI, Rasul et al.Microsystem technologies. 2009, Vol 15, Num 12, pp 1785-1791, issn 0946-7076, 7 p.Article

Effect of spanwise confinement on flag flutter: Experimental measurementsDOARE, Olivier; MANO, David; BILBAO LUDENA, Juan Carlos et al.Physics of fluids (1994). 2011, Vol 23, Num 11, issn 1070-6631, 111704.1-111704.4Article

Oscillatory Behavior of Transonic Aeroelastic Instability BoundariesTIMME, S; BADCOCK, K. J.AIAA journal. 2009, Vol 47, Num 6, pp 1590-1592, issn 0001-1452, 3 p.Article

Flutter characteristics of reentry space vehicle with nonplanar wingKANDA, Atsushi; UEDA, Tetsuhiko; KAI, Takashi et al.AIAA journal. 2006, Vol 44, Num 10, pp 2267-2273, issn 0001-1452, 7 p.Article

Flutter Margins for Multimode Unstable Couplings with Associated Flutter ConfidenceLIND, Rick.Journal of aircraft. 2009, Vol 46, Num 5, pp 1563-1568, issn 0021-8669, 6 p.Article

Identifying parameter-dependent volterra kernels to predict aeroelastic instabilitiesLIND, Rick; PRAZENICA, Richard J; BRENNER, Martin J et al.AIAA journal. 2005, Vol 43, Num 12, pp 2496-2502, issn 0001-1452, 7 p.Article

Experimental Characterization of Limit Cycle Oscillations in Membrane Wing Micro Air VehiclesJOHNSTON, Jordan W; ROMBERG, Will; ATTAR, Peter J et al.Journal of aircraft. 2010, Vol 47, Num 4, pp 1300-1308, issn 0021-8669, 9 p.Article

Basis Vector Quantification of Flutter Analysis Structural ModesNORTHINGTON, Jay S.Journal of aircraft. 2009, Vol 46, Num 6, pp 2107-2114, issn 0021-8669, 8 p.Article