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Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack by Cobleigh, Brent R.

Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model by Cotton, Stacey J.

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Water tunnel flow visualization study of a 4.4% scale X-31 forebody by Cobleigh, Brent R.

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Simultaneous three-dimensional velocity and mixing measurements by use of laser Doppler velocimetry and fluorescence probes in a water tunnel by Neuhart, Dan H. (Dan Howard), 1952-

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Water tunnel flow visualization study through poststall of 12 novel planform shapes / by Gatlin, Gregory M. (Gregory Michael), Neuhart, Dan H. (Dan Howard), 1952-

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Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack / by Cobleigh, Brent R., Croom, Mark A.

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Online Access

Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching by Moreira, J.

Water tunnel flow visualization study through poststall of 12 novel planform shapes by Gatlin, Gregory M.