Computational investigation of step excrescence sensitivity in a swept-wing boundary layer
MW Tufts, HL Reed, BK Crawford, GT Duncan Jr… - Journal of Aircraft, 2017 - arc.aiaa.org
The interaction between an existing stationary crossflow instability and a two-dimensional
step excrescence placed into a swept boundary layer on a lifting surface has been …
step excrescence placed into a swept boundary layer on a lifting surface has been …
Receptivity: the inspiration of Mark Morkovin
HL Reed, WS Saric - 45th AIAA Fluid Dynamics Conference, 2015 - arc.aiaa.org
This paper provides a review of the current findings in receptivity for subsonic/transonic
flows, including a discussion of the origin of the concept via Mark Morkovin, a remarkable …
flows, including a discussion of the origin of the concept via Mark Morkovin, a remarkable …
Flight experiments on the effects of step excrescences on swept-wing transition
GT Duncan Jr, BK Crawford, MW Tufts… - … and Simulation 48, 2014 - inderscienceonline.com
A 30° swept-wing model with a movable, leading-edge extending to 15% chord is used in
flight tests to study the effect of two-dimensional, step excrescences on swept-wing …
flight tests to study the effect of two-dimensional, step excrescences on swept-wing …
Interactive computations and experiments in stability and transition research
HL Reed, TS Kocian, W Saric - 2018 Applied Aerodynamics …, 2018 - arc.aiaa.org
This paper describes results and lessons learned from years of close collaborations
between the authors' computational and experimental groups toward the fundamental …
between the authors' computational and experimental groups toward the fundamental …
Progress in stability and transition research
HL Reed - IUTAM Laminar-Turbulent Transition: 9th IUTAM …, 2022 - Springer
This paper provides an overview of the theoretical and computational boundary-layer
receptivity, stability, and control research conducted by the author over the past four …
receptivity, stability, and control research conducted by the author over the past four …
A Flight Test Technique for Precise Angle-of-Attack Measurements with Application to Laminar Flow Control Flight Research
AA Tucker, WS Saric, HL Reed - 52nd Aerospace Sciences Meeting, 2014 - arc.aiaa.org
Previous flight research programs have sampled laminar flow control (LFC) at a single
control point, usually a cruise condition. In the case of the presently discussed swept-wing …
control point, usually a cruise condition. In the case of the presently discussed swept-wing …