Zobrazeno 1 - 10
of 78
pro vyhledávání: '"Brian R. Hollis"'
Autor:
Brian R. Hollis
Publikováno v:
Journal of Spacecraft and Rockets. 58:1612-1635
An experimental investigation of hexcomb-pattern surface roughness effects on boundary-layer transition and convective heating has been performed. Two representative entry vehicle geometries, a sph...
Publikováno v:
Journal of Thermophysics and Heat Transfer. 33:216-224
A database of heating and pressure measurements on a 7 deg half-angle cone in a high-enthalpy expansion tunnel in CO2 has been generated to support development and validation of computational model...
Autor:
Christopher A. Kuhl, Jay H. Grinstead, Ashley M. Korzun, Gregory T. Swanson, Brian R. Hollis, Aaron M. Brandis, Karl T. Edquist, Carey Fulton Scott, Scott A. Berry, Jose A. Santos, Christopher D. Karlgaard, Milad Mahzari, Brett A. Cruden, Helen H. Hwang, Cole Kazemba, F. McNeil Cheatwood, Christopher O. Johnston, Mark Schoenenberger, Thomas J. Horvath, Ruth Miller
Publikováno v:
Bulletin of the AAS. 53
Autor:
Brian R. Hollis
Publikováno v:
Journal of Spacecraft and Rockets. 59:1-1
Publikováno v:
AIAA AVIATION 2020 FORUM.
Autor:
Brian R. Hollis
Publikováno v:
AIAA Scitech 2020 Forum.
An experimental investigation of hexcomb-pattern surface roughness effects on boundary-layer transition and convective heating has been performed. Two representative entry vehicle geometries, a sph...
Autor:
Brian R. Hollis
Publikováno v:
Journal of Spacecraft and Rockets. 55:856-876
The aerothermodynamic environment of a hypersonic inflatable aerodynamic decelerator with a flexible thermal protection system has been investigated through wind-tunnel testing. Boundary-layer tran...
Publikováno v:
Journal of Thermophysics and Heat Transfer. 31:712-731
An extensive database of heating, pressure, and flowfield measurements on a 70 deg sphere-cone blunt-body geometry in high-enthalpy carbon-dioxide flow has been generated through testing in an expa...
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
A database of heating and pressure measurements on a 7-deg half-angle cone in a highenthalpy expansion tunnel in CO2 has been generated to support development and validation of computational models to be employed in the design of future Mars missions
Autor:
Brian R. Hollis
Publikováno v:
33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference.