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JOURNAL OF AIRCRAFT
Editor-in-Chief :
Thomas M. Weeks

Universal Technology Corporation
Frequency Bimonthly
ISSN 0021-8669
E-ISSN 1533-3868
CURRENT ISSUE
2009 vol. 46 no. 5

Effects of In-Plane Shear Loads on Transverse Shear Deformations in Composite Panels
pages (1473-1478)
doi: 10.2514/1.27913
    Jingbo Wang; James L. Glancey; Jack R. Vinson
Numerical Investigation on Blade/Wake-Interaction Noise Generation
pages (1479-1486)
doi: 10.2514/1.32390
    Y. Mauffrey; G. Rahier; J. Prieur
Evaluation of Computations and Transition Prediction Method for Aircraft High-Lift Configuration
pages (1487-1499)
doi: 10.2514/1.34948
    Mitsuhiro Murayama; Yuzuru Yokokawa; Kazuomi Yamamoto; Yoshine Ueda
Delta Wing Vortex-Burst Behavior Under a Dynamic Freestream
pages (1500-1512)
doi: 10.2514/1.36697
    Ismael Heron; Roy Y. Myose
Elastic Multibody Models of Transport Aircraft High-Lift Mechanisms
pages (1513-1524)
doi: 10.2514/1.37583
    János Zierath; Christoph Woernle; Thomas Heyden
Unified Flutter Solution Technique Using Matrix Singularity Indicators
pages (1525-1532)
doi: 10.2514/1.37985
    Zhichun Yang; Yingsong Gu
Fatigue Life Estimation of Helicopter Landing Probe Based on Dynamic Simulation
pages (1533-1543)
doi: 10.2514/1.38345
    Zheng Hong Zhu; Michael LaRosa; James Ma
Aerothermoacoustic Response of Shape Memory Alloy Hybrid Composite Panels
pages (1544-1555)
doi: 10.2514/1.39214
    Hesham Hamed Ibrahim; Mohammad Tawfik; Hani Mohammed Negm; Hong Hee Yoo
Fatigue Performance of Nitrided Aircraft Crankshafts
pages (1556-1562)
doi: 10.2514/1.39672
    John M. Barsom
Flutter Margins for Multimode Unstable Couplings with Associated Flutter Confidence
pages (1563-1568)
doi: 10.2514/1.40328
    Rick Lind
Calculation of Rotorcraft Inflow Model Coefficients Using Blade Flapping Measurements
pages (1569-1576)
doi: 10.2514/1.40540
    S. S. Houston; D. G. Thomson
Flow past a Yawed Rectangular Cavity in Transonic and Low Supersonic Flows
pages (1577-1583)
doi: 10.2514/1.40729
    B. H. K. Lee; D. M. Orchard; F. C. Tang
Modeling Pilot Control Behavior with Sudden Changes in Vehicle Dynamics
pages (1584-1592)
doi: 10.2514/1.41215
    Ronald A. Hess
Conceptual Design Prediction of the Buffet Envelope of Transport Aircraft
pages (1593-1606)
doi: 10.2514/1.41367
    Adrien Bérard; Askin T. Isikveren
Multistep Results in ICECREMO2
pages (1607-1613)
doi: 10.2514/1.41451
    P. Verdin; J. P. F. Charpin; C. P. Thompson
Identification of a Nonlinear Wing Structure Using an Extended Modal Model
pages (1614-1626)
doi: 10.2514/1.42024
    M. F. Platten; J. R. Wright; J. E. Cooper; G. Dimitriadis
Nonlinear Aircraft Loads in Severe Atmospheric Turbulence
pages (1627-1633)
doi: 10.2514/1.42045
    J. G. Jones
Investigation of Unswept Normal Shock Wave/Turbulent-Boundary-Layer Interaction Control
pages (1634-1641)
doi: 10.2514/1.42104
    Jonathan S. Couldrick; Sudhir L. Gai; John F. Milthorpe; Krishna Shankar
Numerical Simulation of Autorotation in Forward Flight
pages (1642-1648)
doi: 10.2514/1.42209
    Hak Yoon Kim; Dong Jin Sheen; Seung O. Park
Unscented Kalman Filtering for Reentry Vehicle Identification in the Transonic Regime
pages (1649-1659)
doi: 10.2514/1.42256
    A. Vitale; F. Corraro; M. Bernard; G. De Matteis
Effective Block Approach for Aircraft Damage Tolerance Analyses
pages (1660-1666)
doi: 10.2514/1.42306
    W. Z. Zhuang; M. McDonald; M. Phillips; L. Molent
Theoretical Predictions of F-16 Fighter Limit Cycle Oscillations for Flight Flutter Testing
pages (1667-1672)
doi: 10.2514/1.42352
    Earl H. Dowell; Jeffrey P. Thomas; Kenneth C. Hall; Charles M. Denegri
Flying Qualities for a Twin-Jet Transport in Severe Atmospheric Turbulence
pages (1673-1680)
doi: 10.2514/1.42408
    Ray C. Chang; Cun-En Ye; C. Edward Lan; Michael Guan
Three-Degree Decelerating Approaches in High-Density Arrival Streams
pages (1681-1691)
doi: 10.2514/1.42420
    A. M. P. De Leege; A. C. In 't Veld; M. Mulder; M. M. Van Paassen
Value of an Overload Indication System Assessed Through Analysis of Aviation Occurrences
pages (1692-1705)
doi: 10.2514/1.42424
    P. Sartor; D. A. Bond; W. J. Staszewski; R. K. Schmidt
Linear Damage Accumulation for Predicting Fatigue in Fiber Metal Laminates
pages (1706-1713)
doi: 10.2514/1.42486
    S. U. Khan; R. C. Alderliesten; R. Benedictus
Unmanned Air Vehicle Wing-Tip Corona Nonlinear Effect on Atmospheric Electric Field Measurements
pages (1714-1720)
doi: 10.2514/1.42575
    Xingya Da; Huairong Shen; Lei Hong; Rui Zhang
Neural Network Modeling of Lateral Pilot Landing Control
pages (1721-1726)
doi: 10.2514/1.42576
    Ryota Mori; Shinji Suzuki
Three-Dimensional Aerodynamic Simulations of Jumping Paratroopers and Falling Cargo Payloads
pages (1727-1739)
doi: 10.2514/1.42548
    Victor Udoewa
New Supersonic Wing Far-Field Composite-Element Wave-Drag Optimization Method
pages (1740-1758)
doi: 10.2514/1.42823
    Brenda Kulfan
Numerical Evaluation of Limit Cycles of Aeroelastic Systems
pages (1759-1769)
doi: 10.2514/1.42928
    Mauro Manetti; Giuseppe Quaranta; Paolo Mantegazza
Prediction of Helicopter Maneuver Loads Using a Fluid-Structure Analysis
pages (1770-1784)
doi: 10.2514/1.43004
    Jayanarayanan Sitaraman; Beatrice Roget
Numerical Analysis on Aerodynamic Force Generation of Biplane Counter-Flapping Flexible Airfoils
pages (1785-1794)
doi: 10.2514/1.43181
    Jr-Ming Miao; Wei-Hsin Sun; Chang-Hsien Tai
Design and Testing of a Multi-Element Airfoil for Short-Takeoff-and-Landing Ultralight Aircraft
pages (1795-1807)
doi: 10.2514/1.43429
    D. P. Coiro; F. Nicolosi; F. Grasso
Flight Dynamics of High Aspect-Ratio Flying Wings: Effect of Large Trim Deformation
pages (1808-1812)
doi: 10.2514/1.36847
    Brijesh Raghavan; Mayuresh J. Patil
Effect of Mictrotab on Reduction of Noise Due to Aircraft High-Lift Devices
pages (1812-1815)
doi: 10.2514/1.44125
    Brian C. Kuo; Nesrin Sarigul-Klijn
Effects of Surface Flats on the Performance of a Remotely Piloted Aircraft
pages (1815-1818)
doi: 10.2514/1.44124
    Thomas Nix; Kenneth Toro; Lance W. Traub
Dye Visualization of the Flow Structure over a Yawed Nonslender Delta Wing
pages (1818-1822)
doi: 10.2514/1.45274
    C. Canpolat; S. Yayla; B. Sahin; H. Akilli
Comment on “A z-Transform Discrete-Time State-Space Formulation for Aeroelastic Stability Analysis”
pages (1823-1823)
doi: 10.2514/1.44049
    A. Tewari
Reply by the Authors to A. Tewari
pages (1823-1824)
doi: 10.2514/1.46125
    Alexandre Noll Marques; João Luiz F. Azevedo
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