1–20 of 24 hits
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    Hypersonic Wind Tunnel Testing

    Brian R. Hollis | NTRS

    Transition Due to Heat-Shield Cavities on a Mars Entry Vehicle

    Brian R. Hollis / Derek Liechty | AIAA | 2006

    Reply by the Author to Prabhu et al.

    Brian R. Hollis | AIAA | 2003

    Entry, Descent and Landing Seminar Series Wind Tunnel Testing Lecture

    Karen T Berger / Brian R Hollis / Scott A Berry | NTRS

    Mars Sample Return Earth Entry System Woven Roughness Mach 6 Aeroheating Test

    Jonathan S Cheatwood / Christopher O Johnston / Brian R Hollis | NTRS

    Transition Effects on Heating in the Wake of a Blunt Body

    Brian R. Hollis / John N. Perkins | AIAA | 1999

    Turbulent Aeroheating Measurements on a 7-deg Half-Angle Sphere-Cone in a High-Enthalpy CO2 Expansion Tunnel

    Brian R Hollis / Michael D Barnhardt / Matthew Maclean et al. | NTRS | 2018

    FLEET and PLIF Velocimetry Within A Mach 10 Hypersonic Air Flow

    Neil S Rodrigues / Olivia K Tyrrell / Elizabeth F Rieken et al. | NTRS

    FLEET and PLIF Velocimetry Within A Mach 10 Hypersonic Air Flow

    Neil S Rodrigues / Olivia K Tyrrell / Elizabeth F Rieken et al. | NTRS

    Trajectory Reconstruction of the Low-Earth Orbit Flight Test of an Inflatable Decelerator

    Christopher D. Karlgaard / Rohan G. Deshmukh / Soumyo Dutta et al. | NTRS

    Aerothermodynamic Analyses for the LOFTID Technology Demonstration Mission

    Brian R. Hollis / Adam J Wise / Derek S Liechty et al. | NTRS

    X-33 Hypersonic Boundary-Layer Transition

    Scott A. Berry / Thomas J. Horvath / Brian R. Hollis et al. | AIAA | 2001

    X-33 Hypersonic Aerodynamic Characteristics

    Kelly J. Murphy / Robert J. Nowak / Richard A. Thompson et al. | AIAA | 2001

    Aerothermodynamic Analyses for the LOFTID Technology Demonstration Mission

    Brian R. Hollis / Adam J Wise / Derek S Liechty et al. | NTRS

    Computational Study of Hypersonic Transitional Wake Flow

    Robert P. Nance / Brian R. Hollis / Thomas J. Horvath et al. | AIAA | 1999