Spalart–Allmaras with Crossflow Transition Model Using Hamiltonian–Strand Approach
Wind Tunnel Tests on an Outer Wing Segment of the ASW-19X Sailplane
Wind Tunnel Results of the High-Speed NLF(Natural Flow Control)(1)-0213 Airfoil
Vortical Structures on Three-Dimensional Shock Control Bumps
Vortex Flow and Aerodynamic Performance of a Reverse Delta Wing
Verification of a chamberless HLFC design with an outer skin of variable porosity
Validation of the Laboratory Facility for the Nanofluids Forced Convection Research
Validation of Suction Velocity Analysis for Active Laminar Flow Control with Uncertainties
Using Surface Sensitivity from Mesh Adjoint for Transonic Wing Drag Reduction
U.S. Air Force Basic Research in Weakly Ionized Gasdynamics
Unsteady Response of Natural Laminar Flow Airfoil Undergoing Small-Amplitude Pitch Oscillations
Unsteady Flow Transition Effects on a Transonic Laminar Airfoil