Journal of Aircraft

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  Publication Venue For

  • Blade Vibration and Its Effect on the Optimal Performance of Helicopter Rotors.  59:184-195. 2022
  • Enhancement to least square-based approach for time-domain unsteady aerodynamic approximation.  58:111-124. 2021
  • Flutter and limit cycle oscillations of cantilevered plate in supersonic flow.  58:266-278. 2021
  • Nonlinear limit cycle oscillation and flutter analysis of clamped curved plates.  57:368-376. 2020
  • Revisiting the fundamentals of control surface reversal including nonlinear effects.  57:1212-1219. 2020
  • Buffeting and lock in of an airfoil at high angle of attack.  55:771-780. 2018
  • Engineering notes experimental and theoretical flutter investigation for a range of wing wind-tunnel models.  55:891-896. 2018
  • Sound transmission and radiation from a plate-cavity system in supersonic flow.  54:1877-1900. 2017
  • Store-induced limit-cycle oscillations due to nonlinear wing-store attachment.  53:778-789. 2016
  • Landing gear design/maintenance analysis for nonlinear shimmy.  52:1707-1710. 2015
  • Optimum design of compound helicopters that use higher harmonic control.  52:1444-1453. 2015
  • Stability of rectangular plates in subsonic flow with various boundary conditions.  52:439-451. 2015
  • Aeroelastic model of multisegmented folding wings: Theory and experiment.  49:911-921. 2012
  • Reduced-order modeling of flutter and limit-cycle oscillations using the sparse volterra series.  49:1803-1812. 2012
  • Aeroelastic analysis and experiment for wing/store model with stiction nonlinearity.  48:1512-1530. 2011
  • Computational evaluation of the performance of lifting surfaces with leading-edge protuberances.  48:591-600. 2011
  • Structural Dynamics model of multisegmented folding wings: Theory and experiment.  48:2149-2160. 2011
  • Comparison of theoretical structural models with experiment for a high-aspect-ratio aeroelastic wing.  46:708-713. 2009
  • Improved flutter boundary prediction for an isolated two-degree-of-freedom airfoil.  46:2069-2076. 2009
  • Improving precision vertical flight operations through a direct-perception-action display.  46:1270-1279. 2009
  • Theoretical predictions of F-16 fighter limit cycle oscillations for flight flutter testing.  46:1667-1672. 2009
  • Delta wing with store limit-cycle-oscillation modeling using a high-fidelity structural model.  45:1054-1061. 2008
  • Theoretical and experimental aeroelastic study for folding wing structures.  45:1136-1147. 2008
  • Aerodynamic loading for an airfoil with an oscillating gurney flap.  44:1245-1257. 2007
  • Experimental evaluation of sinusoidal leading edges.  44:1404-1408. 2007
  • Aerodynamic flow control of an airfoil with small trailing-edge strips.  43:1854-1866. 2006
  • Erratum: Stochastic analysis of a nonlinear aeroelastic model using the response surface method (Journal of Aircraft (2006) (1044)).  43:1959. 2006
  • Flutter and limit-cycle oscillations for a wing-store model with freeplay.  43:487-503. 2006
  • Stochastic analysis of a nonlinear aeroelastic model using the response surface method.  43:1044-1052. 2006
  • Modeling delta wing limit-cycle oscillations using a high-fidelity structural model.  42:1209-1217. 2005
  • Worst-case gust-response analysis for typical airfoil section with control surface.  42:956-962. 2005
  • Aeroelastic wing with leading- and trailing-edge control surfaces.  40:559-565. 2003
  • Compact methodology for computing limit-cycle oscillations in aeroelasticity.  40:955-963. 2003
  • Constructal theory: Tree-shaped flows and energy systems for aircraft.  40:43-48. 2003
  • Nonlinear aeroelasticity.  40:857-874. 2003
  • Limit-cycle hysteresis response for a high-aspect-ratio wing model.  39:885-888. 2002
  • Control of a three-degree-of-freedom airfoil with limit-cycle behavior.  37:533-536. 2000
  • Nonlinear aeroelastic response of delta wing to periodic gust.  37:155-164. 2000
  • Experimental active control of a typical section using a trailing-edge flap.  35:224-229. 1998
  • Reduced-order aerodynamic model and its application to a nonlinear aeroelastic system.  35:332-338. 1998
  • Unsteady aerodynamic forces and aeroelastic response for external store of an aircraft.  35:678-687. 1998
  • Nonlinear rotor aeroelastic analysis with stall and advanced wake dynamics.  34:679-687. 1997
  • Active control of panel flutter with piezoelectric transducers.  33:768-774. 1996
  • Damping prediction for hingeless rotor aeroelastic stability with experimental correlation.  33:1071-1078. 1996
  • Experiments and analysis for a gust generator in a wind tunnel.  33:139-148. 1996
  • Flow about a slotted cylinder-airfoil combination in a wind tunnel.  33:716-721. 1996
  • State-space modeling for aeroelastic panels with linearized potential flow aerodynamic loading.  33:816-822. 1996
  • Experimental investigation of three-dimensional dynamic stall model oscillating in pitch.  32:1062-1071. 1995
  • Response of a nonrotating rotor blade to lateral turbulence Part II: Experiment.  32:154-160. 1995
  • Response of a nonrotating rotor blade to lateral turbulence part I: Theory.  32:145-153. 1995
  • Helicopter rotor lift distributions for minimum-induced power loss.  31:837-845. 1994
  • Flutter and stall response of a helicopter blade with structural nonlinearity.  29:953-960. 1992
  • New device for controlling asymmetric flowfields on forebodies at large alpha.  28:456-462. 1991
  • Combined effects of nose bluntness and surface perturbations on asymmetric flow past slender bodies.  27:909-910. 1990
  • New free-wake analysis of rotorcraft hover performance using influence coefficients.  26:1090-1097. 1989
  • Damping in beams with multiple dry friction supports.  24:820-832. 1987
  • Forebody vortex management for yaw control at high angles of attack.  24:248-254. 1987
  • Influence of nonlinear blade damping on helicopter ground resonance instability.  23:104-110. 1986
  • Flutter analysis using nonlinear aerodynamic forces.  21:101-109. 1984
  • Effect of unsteady forcing on the sinusoidal instability of vortex wakes.  19:713-721. 1982
  • Interior noise studies for single- and double-walled cylindrical shells.  17:690-699. 1980
  • Structural analysis of a cooled, directionally solidified turbine blade.  14:167-172. 1977
  • Modeling engine static structures with conical shell finite elements.  12:230-233. 1975
  • Aerodynamic boundary layer effects on flutter and damping of plates.  10:734-738. 1973
  • Incipient stall detection through unsteady-pressure monitoring on aircraft wings.  9:186-188. 1972
  • Computational study of aeroelastic limit cycles due to localized structural nonlinearities 2018