W. Goad

Recent flow visualization studies in the 0.3-m TCT

A. W. Burner, W. L. Snow, W. Goad, 1987 .

FLEET Velocimetry in the Common Research Model’s Wing Wake

Melissa B. Rivers, Eric L. Walker, P. Danehy, 2020, AIAA Scitech 2020 Forum.

Model Deformation Measurements at a Cryogenic Wind Tunnel Using Photogrammetry

A. W. Burner, Walter L. Snow, W. K. Goad, 1982 .

Measuring Global Surface Pressures on a Circulation Control Concept Using Pressure Sensitive Paint

W. K. Goad, Kyle Z. Goodman, Bradley D. Leighty, 2012 .

Results From a Pressure Sensitive Paint Test Conducted at the National Transonic Facility on Test 197: The Common Research Model

A. Neal Watkins, W. K. Goad, Kyle Z. Goodman, 2011 .

The Development and Implementation of a Cryogenic Pressure Sensitive Paint System in the National Transonic Facility

A. Neal Watkins, Donald M. Oglesby, Kyle Z. Goodman, 2009 .

Flow Visualization at Cryogenic Conditions Using a Modified Pressure Sensitive Paint Approach

Odis C. Pendergraft, Richard L. Campbell, Clifford J. Obara, 2005 .