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    Flow-Field Measurements in a Wing-Fuselage Junction Using an Embedded Particle Image Velocimetry System

    Jenkins, Luther N. / Yao, Chung-Sheng / Bartram, Scott M. | AIAA | 2019

    Update on the Juncture Flow PIV Results and Future Plans

    Jenkins, Luther N. / Yao, Chung-Sheng / Bartram, Scott M. | NTRS | 2019

    A Comparative Study of Simulated and measured Gear-Flap Flow Interaction

    Khorrami, Mehdi R. / Mineck, Raymond E. / Fares, Ehab et al. | AIAA | 2015

    Trapezoidal Wing Experimental Repeatability and Velocity Profiles in the 14- by 22-Foot Subsonic Tunnel

    Hannon, Judith A. / Washburn, Anthony E. / Jenkins, Luther N. et al. | NTRS | 2012

    Stability and Control Properties of an Aeroelastic Fixed Wing Micro Aerial Vehicle

    Waszak, Martin R. / Jenkins, Luther N. / Ifju, Peter | NTRS | 2001

    Low-speed Aerodynamic Investigations of a Hybrid Wing Body Configuration

    Vicroy, Dan D. / Gatlin, Gregory M. / Jenkins, Luther N. et al. | AIAA | 2014

    Unsteady flowfield around tandem cylinders as prototype component interaction in airframe noise

    Khorrami, Mehdi R. / Choudhari, Meelan M. / Lockard, David P. et al. | Tema Archiv | 2007

    Contributions of Particle Image Velocimetry to Helicopter Aerodynamics

    Raffel, Markus / Bauknecht, André / Ramasamy, Manikandan et al. | AIAA | 2017

    Experimental Investigation of Rotorcraft Outwash in Ground Effect

    Tanner, Philip E. / Overmeyer, Austin D. / Jenkins, Luther N. et al. | NTRS | 2015

    Flow-Field Investigation of Gear-Flap Interaction on a Gulfstream Aircraft Model

    Yao, Chung-Sheng / Jenkins, Luther N. / Bartram, Scott M. et al. | AIAA | 2014

    Experimental investigation of vortex-fin interaction

    Washburn, Anthony E. / Jenkins, Luther N. / Ferman, Marty A. | NTRS | 1993

    Boundary Condition Study for the Juncture Flow Experiment in the NASA Langley 14x22-Foot Subsonic Wind Tunnel

    Rumsey, Christopher L. / Carlson, Jan-Renee / Hannon, Judith A. et al. | AIAA | 2017

    Flow-Field Investigation of Gear-Flap Interaction on a Gulfstream Aircraft Model

    Yao, Chung-Sheng / Jenkins, Luther N. / Bartram, Scott M. et al. | NTRS | 2014

    Active Aerodynamic Load Reduction on a Rotorcraft Fuselage With Rotor Effects: A CFD Validation Effort

    Allan, Brian G. / Schaeffler, Norman W. / Jenkins, Luther N. et al. | NTRS | 2015

    Projection Moire Interferometry Measurements of Micro Air Vehicle Wings

    Fleming, Gary A. / Bartram, Scott M. / Waszak, Martin R. et al. | NTRS | 2001

    Development of a Large Field-of-View PIV System for Rotorcraft Testing in the 14- x 22-Foot Subsonic Tunnel

    Jenkins, Luther N. / Yao, Chung-Sheng / Bartram, Scott M. et al. | NTRS | 2009

    An Active Flow Circulation Controlled Flap Concept for General Aviation Aircraft Applications

    Jones, Gregory S. / Viken, Sally A. / Washburn, Anthony E. et al. | NTRS | 2002

    Mechanisms of Active Aerodynamic Load Reduction on a Rotorcraft Fuselage With Rotor Effects

    Schaeffler, Norman W. / Allan, Brian G. / Jenkins, Luther N. et al. | NTRS | 2016