Richard A. Wahls

发表

Summary Data from the Sixth AIAA CFD Drag Prediction Workshop: CRM Cases

Edward N. Tinoco, Olaf Brodersen, Stefan Keye, 2017, Journal of Aircraft.

Summary of Data from the Sixth AIAA CFD Drag Prediction Workshop: CRM Cases 2 to 5

Edward N. Tinoco, Olaf Brodersen, Stefan Keye, 2017 .

Results from the Second AIAA Computational Fluid Dynamics Drag Prediction Workshop

Edward N. Tinoco, Olaf Brodersen, Kelly R. Laflin, 2005 .

AIAA 2002-0841 Summary of Data from the

Richard A. Wahls, Shahyar Pirzadeh, Michael J. Hemsch, 2002 .

Forced Transition Techniques on HSCT Configurations

Richard A. Wahls, Lewis R. Owens, Steven X. S. Bauer, 1999 .

Boundary Layer Transition in the NTF: HSR Experience and Plans

Richard A. Wahls, Lewis R. Owens, Marvine Hamner, 1999 .

Grid Quality and Resolution Issues from the Drag Prediction Workshop Series

Edward N. Tinoco, Olaf Brodersen, John C. Vassberg, 2008 .

Summary of the Fourth AIAA CFD Drag Prediction Workshop

Edward N. Tinoco, Olaf Brodersen, John C. Vassberg, 2010 .

Recent Enhancements to the National Transonic Facility (Mixed Mode Operations)

Richard A. Wahls, David Chan, S. Balakrishna, 2006 .

Testing the 2.2% HSR Reference H Model with a Modified Wing Planform in the NTF

Richard A. Wahls, Lewis R. Owens, Marvine Hamner, 1999 .

Off-Design Reynolds Number Effects for a Supersonic Transport

Richard A. Wahls, S. Melissa Rivers, Lewis R. Owens, 2013 .

Retrospective on the Common Research Model for Computational Fluid Dynamics Validation Studies

Richard A. Wahls, Mark A. DeHaan, John C. Vassberg, 2018, Journal of Aircraft.

Summary of Data from the Fifth Computational Fluid Dynamics Drag Prediction Workshop

Edward N. Tinoco, Olaf Brodersen, Kelly R. Laflin, 2014 .

Development of a Common Research Model for Applied CFD Validation Studies

John C. Vassberg, Richard A. Wahls, Mark A. DeHaan, 2008 .

Aftbody Closure Effects on the Reference H Configuration at Subsonic and Transonic Speeds

Richard A. Wahls, Lewis R. Owens, W. Kelly Londenberg, 1999 .

Initial Results of Reynolds Number Testing at LaRC's NTF Using the 2.2% Reference H Model

Richard A. Wahls, Lewis R. Owens, Marvine Hamner, 1999 .

Focused Assessment of State-of-the-Art CFD Capabilities for Prediction of Subsonic Fixed Wing Aircraft Aerodynamics

Richard A. Wahls, Christopher L. Rumsey, C. Rumsey, 2008 .

Next Generation Civil Transport Aircraft Design Considerations for Improving Vehicle and System-Level Efficiency

Richard A. Wahls, Mark D. Guynn, Ruben DelRosario, 2013 .

Summary of the Fourth AIAA Computational Fluid Dynamics Drag Prediction Workshop

Edward N. Tinoco, Olaf Brodersen, John C. Vassberg, 2014 .

Grid Quality and Resolution Issues from the Drag Prediction Workshop Series

Edward N. Tinoco, Olaf Brodersen, John C. Vassberg, 2008 .

High Reynolds Number Effects on HSCT Stability and Control Characteristics

Richard A. Wahls, Douglas L. Wilson, Lewis R. Owens, 1999 .

NASA's Fundamental Aeronautics Subsonic Fixed Wing Project: Generation N+3 Technology Portfolio

Richard A. Wahls, Ruben Del Rosario, Gregory J. Follen, 2011 .

Summary of Data from the Fifth AIAA CFD Drag Prediction Workshop

Edward N. Tinoco, Olaf Brodersen, Kelly R. Laflin, 2013 .

Fixed Wing Project: Technologies for Advanced Air Transports

Richard A. Wahls, Ruben Del Rosario, John M. Koudelka, 2014 .

Fuel Efficiencies Through Airframe Improvements

Anthony E. Washburn, Richard A. Wahls, Mark F. Mangelsdorf, 2011 .

Data Summary from Second AIAA Computational Fluid Dynamics Drag Prediction Workshop

Edward N. Tinoco, Olaf Brodersen, Kelly R. Laflin, 2003 .

Summary of Data from the Second AIAA CFD Drag Prediction Workshop (Invited)

Edward N. Tinoco, Olaf Brodersen, Kelly R. Laflin, 2004 .

Investigation of Transonic Reynolds Number Scaling on a Twin-Engine Transport

Richard A. Wahls, O. C. Pendergraft, D. R. Bogue, 2002 .

Plans and Progress in the research of Subsonic Transports under NASA's Subsonic Fixed Wing and Environmentally Responsible Aviation Projects

Richard A. Wahls, Ruben Del Rosario, 2009 .

Total Technology Readiness Level: Accelerating Technology Readiness for Aircraft Design

Richard A. Wahls, Michael L. Drake, Jeanne C. Yu, 2021, AIAA AVIATION 2021 FORUM.

Summary of Data from the First AIAA CFD Drag Prediction Workshop

John C. Vassberg, Richard A. Wahls, Shahyar Pirzadeh, 2002 .

Finite-difference outer-layer, analytic inner-layer method for turbulent boundary layers

Richard A. Wahls, Fred R. Dejarnette, Richard W. Barnwell, 1989 .

Use of Boundary Layer Transition Detection to Validate Full-Scale Flight Performance Predictions

Richard A. Wahls, David Yeh, Lewis R. Owens, 1999 .

Abridged Summary of the Third AIAA Computational Fluid Dynamics Drag Prediction Workshop

Edward N. Tinoco, Olaf Brodersen, Kelly R. Laflin, 2008 .

Prediction and Assessment of Reynolds Number Sensitivities Associated with Wing Leading-Edge Radius Variations

Richard A. Wahls, Melissa B. Rivers, Lewis R. Owen, 1999 .

Investigations for Supersonic Transports at Transonic and Supersonic Conditions

Richard A. Wahls, Lewis R. Owens, S. M. B. Rivers, 2008 .

Reynolds Number Effects on the Stability and Control Characteristics of a Supersonic Transport

Richard A. Wahls, Lewis R. Owens, Marvine Hamner, 2002 .

Reynolds number effects on off-design stability and control characteristics of supersonic transports

Richard A. Wahls, Lewis R. Owens, Marvine Hamner, 2007 .