T. Horvath

发表

Overview of Boundary Layer Transition Research in Support of Orbiter Return To Flight

Scott A. Berry, Thomas J. Horvath, Francis A. Greene, 2006 .

Discrete Roughness Transition for Hypersonic Flight Vehicles

S. Berry, T. Horvath, 2007 .

- 2010-243 Cast Glance Near Infrared Imaging Observations of th Space Shuttle During Hypersonic Re-entry

T. Horvath, Steve Tack, D. Tomek, 2010 .

Shuttle Damage/Repair from the Perspective of Hypersonic Boundary Layer Transition - Experimental Results

Karen T. Berger, S. Berry, T. Horvath, 2006 .

HYTHIRM Radiance Modeling and Image Analyses in Support of STS-119, STS-125 and STS-128 Space Shuttle Hypersonic Re-entries

Alan B. Tietjen, Jeff C. Taylor, T. Horvath, 2010 .

Hypersonic Boundary/Shear Layer Transition for Blunt to Slender Configurations - A NASA Langley Experimental Perspective

Scott A. Berry, Thomas J. Horvath, N. Merski, 2004 .

Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6 Wind Tunnels

Scott A. Berry, Thomas J. Horvath, Brian R. Hollis, 2002 .

Reynolds number influences in aeronautics

Pierce L. Lawing, Thomas J. Horvath, Long P. Yip, 1993 .

Coherent Shedding from a Circular Cylinder at Critical, Supercritical, and Transcritical Reynolds Numbers

Thomas J. Horvath, Gregory S. Jones, T. Horvath, 1986 .

X-33 Hypersonic Boundary Layer Transition

Scott A. Berry, Thomas J. Horvath, Richard A. Thompson, 1999 .

X-33 Turbulent Aeroheating Measurements and Predictions

S. Berry, T. Horvath, B. Hollis, 2002 .

AIAA 2002-4700 X-33 Turbulent Aeroheating Measurements and Predictions

S. Berry, T. Horvath, B. Hollis, 2002 .

Computational/Experimental Aeroheating Predictions for X-33. Phase 2; Vehicle

Scott A. Berry, Thomas J. Horvath, K. James Weilmuenster, 1998 .

Computational study of hypersonic transitional wake flow

Stephen J. Alter, T. Horvath, R. Nance, 1999 .

AIAA 99-3559 X-33 Computational Aeroheating Predictions and Comparisons

Stephen J. Alter, S. Berry, T. Horvath, 1999 .

X-33 Rev-F Turbulent Aeroheating Results From Test 6817 in NASA Langley 20-Inch Mach 6 Air Tunnel and Comparisons With Computations

S. Berry, T. Horvath, B. Hollis, 2003 .

Planetary Rover Robotics Experiment in Education: Carbonate Rock Collecting Experiment of the Husar-5 Rover of the Széchenyi István High School, Sopron, Hungary

T. Horvath, S. Bérczi, P. Prajczer, 2013 .

Aerothermal Testing for Project Orion Crew Exploration Vehicle

Scott A. Berry, Thomas J. Horvath, Randolph P. Lillard, 2009 .

Protuberance Boundary Layer Transition for Project Orion Crew Entry Vehicle

Adam J. Amar, Scott A. Berry, Thomas J. Horvath, 2008 .

Application of a Near Infrared Imaging System for Thermographic Imaging of the Space Shuttle during Hypersonic Re-Entry

Thomas J. Horvath, Brett C. Bush, C. David Mercer, 2010 .

X-33 Computational Aeroheating/Aerodynamic Predictions and Comparisons With Experimental Data

Scott A. Berry, Thomas J. Horvath, Richard A. Thompson, 2003 .

Comparison of Methods for Determining Boundary Layer Edge Conditions for Transition Correlations

Scott A. Berry, Thomas J. Horvath, Brian R. Hollis, 2003 .

X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography

Howard H. Hamilton, Scott A. Berry, Thomas J. Horvath, 1999 .

1 X-33 HYPERSONIC BOUNDARY LAYER TRANSITION

Richard A. Thompson, S. Berry, T. Horvath, 1999 .

Roles of Engineering Correlations in Hypersonic Entry Boundary Layer Transition Prediction

Charles H. Campbell, Scott A. Berry, Thomas J. Horvath, 2010 .

Blunt body near-wake flow field at Mach 10

Thomas J. Horvath, Klaus Hannemann, T. Horvath, 1997 .

Entry, Descent, and Landing Aerothermodynamics: NASA Langley Experimental Capabilities and Contributions

Scott A. Berry, Thomas J. Horvath, Shann J. Rufer, 2014 .

A System Trade Study of Remote Infrared Imaging for Space Shuttle Reentry

Scott A. Berry, Thomas J. Horvath, Richard J. Schwartz, 2008 .

X-38 Experimental Aerothermodynamics

Scott A. Berry, Thomas J. Horvath, N. Ronald Merski, 2004 .

X-33 (Rev-F) Aeroheating Results of Test 6770 in NASA Langley 20-Inch Mach 6 Air Tunnel

Scott A. Berry, Thomas J. Horvath, Derek S. Liechty, 1999 .

AIAA 98-0881 X-34 EXPERIMENTAL AEROHEATING AT MACH 6 AND 10

Scott A. Berry, Thomas J. Horvath, Michael DiFulvio, 1998 .

1 X-38 Experimental Aeroheating at Mach 10

Stephen J. Alter, S. Berry, T. Horvath, 2001 .

Shuttle Entry Imaging Using Infrared Thermography

Scott A. Berry, Thomas J. Horvath, Martin Ross, 2007 .

A Vision of Quantitative Imaging Technology for Validation of Advanced Flight Technologies

Thomas J. Horvath, David M. Gibson, Jay H. Grinstead, 2011 .

Aeroheating Testing and Predictions for Project Orion Crew Exploration Vehicle

Thomas J. Horvath, Benjamin S. Kirk, Brian R. Hollis, 2009 .

X-38 Experimental Aeroheating At Mach 10

Stephen J. Alter, S. Berry, T. Horvath, 2001 .

Experimental and computational studies of the flow over a sting mounted planetary probe configuration

Thomas J. Horvath, Iain D. Boyd, John K. Harvey, 1997 .

Mars Sample Return Orbiter

Thomas J. Horvath, Peter A. Gnoffo, F. McNeil Cheatwood, 2001 .

Aerothermodynamic measurements on a proposed assured crew return vehicle (ACRV) lifting-body configuration at Mach 6 and 10 in air

Thomas J. Horvath, Matthew N. Rhode, Gregory M. Buck, 1990 .

Cast Glance Near Infrared Imaging Observations of the Space Shuttle During Hypersonic Re-Entry

Thomas J. Horvath, Harry A. Verstynen, Deborah M. Tomek, 2010 .

X-34 Experimental Aeroheating at Mach 6 and 10

Scott A. Berry, Thomas J. Horvath, Michael DiFulvio, 1998 .

American Institute of Aeronautics and Astronautics 1 Flight Experiment Verification of Shuttle Boundary Layer Transition Prediction Tool

Scott A. Berry, Thomas J. Horvath, Karen T. Berger, 2016 .

Assessment and Mission Planning Capability For Quantitative Aerothermodynamic Flight Measurements Using Remote Imaging

Scott A. Berry, Thomas J. Horvath, Richard J. Schwartz, 2008 .

Boundary Layer Control for Hypersonic Airbreathing Vehicles

Scott A. Berry, Thomas J. Horvath, Robert J. Nowak, 2004 .