Heath B. Johnson, Ph.D.

Affiliations: 
2000 University of Minnesota, Twin Cities, Minneapolis, MN 
Area:
Aerospace Engineering
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"Heath Johnson"

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Graham V. Candler grad student 2000 UMN
 (Thermochemical interactions in hypersonic boundary layer stability.)
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Publications

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Wartemann V, Wagner A, Wagnild R, et al. (2019) High-Enthalpy Effects on Hypersonic Boundary-Layer Transition Journal of Spacecraft and Rockets. 56: 347-356
Riley ZB, McNamara JJ, Johnson HB. (2014) Assessing hypersonic boundary-layer stability in the presence of structural deformation Aiaa Journal. 52: 2547-2558
Gronvall JE, Johnson HB, Candler GV. (2014) Boundary-Layer Stability Analysis of the High Enthalpy Shock Tunnel Transition Experiments Journal of Spacecraft and Rockets. 51: 455-467
Gosse R, Kimmel R, Johnson HB. (2014) Study of Boundary-Layer Transition on Hypersonic International Flight Research Experimentation 5 Journal of Spacecraft and Rockets. 51: 151-162
Casper KM, Johnson HB, Schneider SP. (2011) Effect of freestream noise on roughness-induced transition for a slender cone Journal of Spacecraft and Rockets. 48: 406-413
Berger KT, Greene FA, Kimmel R, et al. (2009) Erratum on "Aerothermodynamic Testing and Boundary-Layer Trip Sizing of the HIFire Flight 1 Vehicle" Journal of Spacecraft and Rockets. 46: 473-480
Berger KT, Greene FA, Kimmel R, et al. (2008) Aerothermodynamic testing and boundary-layer trip sizing of the HIFiRE flight 1 vehicle Journal of Spacecraft and Rockets. 45: 1117-1124
MacLean M, Wadhams T, Holden M, et al. (2008) Ground Test Studies of the HIFiRE-1 Transition Experiment Part 2: Computational Analysis Journal of Spacecraft and Rockets. 45: 1149-1164
Alba CR, Johnson HB, Bartkowicz MD, et al. (2008) Boundary-layer stability calculations for the HIFiRE-1 transition experiment Journal of Spacecraft and Rockets. 45: 1125-1133
Johnson H, Alba C, Candler G, et al. (2008) Boundary-Layer Stability Analysis of the Hypersonic International Flight Research Transition Experiments Journal of Spacecraft and Rockets. 45: 228-236
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