61–80 von 1,043 Ergebnissen
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    Modeling of Asymmetric Elevator Failures in the F-16 Aircraft

    Gumusboga, Ilkay / Iftar, Altug | AIAA | 2019

    PAB3D Simulations for the CAWAPI F-16XL

    Elmiligui, Alaa / Massey, Steven / Abdol-Hamid, Khaled | AIAA | 2007

    F-22 Actuator Dynamic Stiffness (Impedance) Testing

    Layton, David / Gaines, Vatanna | AIAA | 2007

    A description of the F/A-18E/F design and design process

    Young, James / Anderson, Ronald / Yurkovich, Rudolph | AIAA | 1998

    Prediction of Buffet Loads of F-15 with FUN3D Solver

    Yang, Shuchi / Chen, Ping-Chih / Wang, Xiaoquan et al. | AIAA | 2016

    Aerodynamics of the F-15 At High Angle of Attack

    Yang, Shuchi / Chen, Ping-Chih / Wang, Xq et al. | AIAA | 2015

    Development of the F/A-18 E/F air induction system

    HALL, G. / HURWITZ, W. / TIEBENS, G. et al. | AIAA | 1993

    Acoustical Environment of an F-35B During Vertical Landings

    Reichman, Brent O. / Downing, J. M. / James, Michael M. et al. | AIAA | 2015

    F-16 Limit-Cycle Oscillation Analysis Using Nonlinear Damping

    Denegri, Charles M. / Sharma, Vinod K. / Northington, Jay S. | AIAA | 2015

    F-22 Aeroelastic Design and Test Validation

    Anderson, William / Mortara, Sean | AIAA | 2007

    Design and Simulation of F/A-18A Automatic Carrier Landing Guidance Controller

    Yue, Liuming / Liu, Gang / Hong, Guanxin | AIAA | 2016

    F-16 Wing Structural Deflection Testing - Phase I

    Northington, Jay / Pasiliao, Crystal | AIAA | 2007

    Optimizing Hot-Surface-Assisted Ignition Performance of High-Pressure F-24 Fuel Sprays

    Motily, Austen / Wood, Eric J. / Ryu, Je Ir et al. | AIAA | 2021

    Toward an Efficient Method for F-16 Limit Cycle Oscillation Prediction

    Kariv, Daniel / Kunz, Donald L. / Iovnovich, Michael | AIAA | 2023

    F-22 Raptor GBU-39 Separation Test Results

    Kummer, Gerald / Besson, Micah / Gunnett, Adam et al. | AIAA | 2011

    Detached Eddy Simulation of the Reentry-F Flight Experiment

    Barnhardt, Michael / Candler, Graham | AIAA | 2008

    Research on the F/A-18E/F using a 22 percent-dynamically-scaled drop model

    Croom, Mark / Kenney, Holly / Murri, Daniel et al. | AIAA | 2000