Lift-TO-Drag Ratios of Slender Wings at Hypersonic Speeds
High‐Speed Aeroelastic Nonlinearities
Two-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
One-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
Drag Reduction and Aerodynamic Shape Optimization for Spike-Tipped Supersonic Blunt Nose
Maximum lift-to-drag ratio of a slender wing at hypersonic speeds.
Flight Experiment Verification of Shuttle Boundary Layer Transition Prediction Tool
Maximum Lift-TO-Drag Ratios of a Slender, Flat-Top, Hypersonic Bodies, Part 1
Simulations of Ash and Sand Impact on a Hypersonic Forebody