NASA Langley Experimental Aerothermodynamic Contributions to Slender and Winged Hypersonic Vehicles

[1]  John Micol,et al.  Langley Aerothermodynamic Facilities Complex: Enhancements and Testing Capabilities , 1998 .

[2]  Shann J. Rufer,et al.  Experimental and Computational Study of Underexpanded Jet Impingement Heat Transfer , 2009 .

[3]  Scott A. Berry,et al.  AIAA 98-0881 X-34 EXPERIMENTAL AEROHEATING AT MACH 6 AND 10 , 1998 .

[4]  Richard A. Thompson,et al.  X-33 Aerodynamic Computations and Comparisons with Wind-Tunnel Data , 2001 .

[5]  J. H. Thomas,et al.  Hypersonic Boundary Layer Transition for the X-33 Phase II Vehicle , 1998 .

[6]  Kathryn E. Wurster,et al.  Effect of Computational Method on Discrete Roughness Correlations for Shuttle Orbiter , 2006 .

[7]  Scott A. Berry,et al.  Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness , 1998 .

[8]  Paul M. Danehy,et al.  Planar laser-induced fluorescence (PLIF) investigation of hypersonic flowfields in a Mach 10 wind tunnel (invited) , 2006 .

[9]  Gregory M. Buck,et al.  Rapid Model Fabrication and Testing for Aerospace Vehicles , 2000 .

[10]  Scott A. Berry,et al.  Review of Orbiter Flight Boundary Layer Transition Data , 2006 .

[11]  Merski N. Ronald.  Reduction and Analysis of Phosphor Thermography Data With the IHEAT Software Package , 1998 .

[12]  Joel L. Everhart,et al.  Turbulent Supersonic/Hypersonic Heating Correlations for Open and Closed Cavities , 2009 .

[13]  Scott A. Berry,et al.  Overview of Boundary Layer Transition Research in Support of Orbiter Return To Flight , 2006 .

[14]  Scott A. Berry,et al.  Boundary Layer Transition Results From STS-114 , 2006 .

[15]  Thomas J. Horvath,et al.  Aerothermodynamic measurements on a proposed assured crew return vehicle (ACRV) lifting-body configuration at Mach 6 and 10 in air , 1990 .

[16]  C Engelund Walter,et al.  Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Propulsion Experiments , 2000 .

[17]  J Brauckmann Gregory,et al.  X-34 Vehicle Aerodynamic Characteristics , 1998 .

[18]  S. Berry,et al.  Discrete Roughness Transition for Hypersonic Flight Vehicles , 2007 .

[19]  Scott A. Berry,et al.  X-38 Experimental Aeroheating At Mach 10 , 2004 .

[20]  Michael DiFulvio,et al.  Hyper-X Stage Separation Wind-Tunnel Test Program , 2001 .

[21]  Scott A. Berry,et al.  Computational/Experimental Aeroheating Predictions for X-33. Phase 2; Vehicle , 1998 .

[22]  Scott A. Berry,et al.  Hypersonic Boundary-Layer Trip Development for Hyper-X , 2000 .

[23]  Scott A. Berry,et al.  X-33 Hypersonic Boundary Layer Transition , 1999 .

[24]  John Micol,et al.  Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center - Aerothermodynamic Facilities Complex , 1995 .

[25]  Kim S. Bey,et al.  Assessment of LAURA for Laminar Supersonic Shallow Cavities , 2004 .

[26]  Kathryn E. Wurster,et al.  Boundary-Layer Transition on X-43A , 2010 .

[27]  Roger L. Kimmel,et al.  Aerothermodynamic Testing and Boundary-Layer Trip Sizing of the HIFiRE Flight 1 Vehicle , 2008 .

[28]  Roger L. Kimmel,et al.  HIFiRE-1 Background and Lessons Learned , 2012 .

[29]  Charles H. Campbell,et al.  Infrared Imaging of Boundary Layer Transition Flight Experiments , 2008 .

[30]  John W. Paulson,et al.  Experimental and Computational Analysis of Shuttle Orbiter Hypersonic Trim Anomaly , 1995 .

[31]  C G Miller,et al.  Aerothermodynamic Flight Simulation Capabilities for Aerospace Vehicles , 1998 .

[32]  Roger L. Kimmel,et al.  HIFiRE-1 Data Analysis: Boundary Layer Transition Experiment During Reentry , 2012 .

[33]  Roger L. Kimmel,et al.  Aerothermodynamic Characteristics of Boundary Layer Transition and Trip Effectiveness of the HIFiRE Flight 5 Vehicle , 2009 .

[34]  N Pamadi Bandu,et al.  Aerodynamic Characteristics, Database Development and Flight Simulation of the X-34 Vehicle , 2000 .

[35]  Scott A. Berry,et al.  Orbiter Boundary Layer Transition Prediction Tool Enhancements , 2010 .

[36]  Arthur C. Grantz,et al.  X-37B Orbital Test Vehicle and Derivatives , 2011 .

[37]  Scott A. Berry,et al.  X-38 Experimental Aerothermodynamics , 2004 .

[38]  K Prabhu Ramadas,et al.  X-33 Hypersonic Aerodynamic Characteristics , 1999 .

[39]  Joel L. Everhart.  Supersonic/Hypersonic Laminar Heating Correlations for Rectangular and Impact-Induced Open and Closed Cavities , 2008 .

[40]  J. H. Thomas,et al.  X-33 Computational Aeroheating Predictions and Comparisons With Experimental Data , 1999 .

[41]  Thomas J. Horvath.  Experimental Aerothermodynamics In Support Of The Columbia Accident Investigation , 2004 .

[42]  Scott A. Berry,et al.  Isolated Roughness Induced Boundary-Layer Transition: Shuttle Orbiter Ground Tests and Flight Experience , 1997 .

[43]  Karen T. Berger,et al.  Shuttle Damage/Repair from the Perspective of Hypersonic Boundary Layer Transition - Experimental Results , 2006 .

[44]  Charles H. Campbell,et al.  Orbiter Return-To-Flight Entry Aeroheating , 2006 .