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Secondary Side Considerations for Boundary Layer Transition Flight Experiment
Two-Dimensional Ablation and Thermal Response Analyses for Mars Science Laboratory Heat Shield
Effect of Freestream Noise on Hypersonic Crossflow-Induced Boundary-Layer Transition
Performance of a hydrofoil operating close to a free surface over a range of angles of attack
Flow Separation Control by Plasma Actuator with Nanosecond Pulsed-Periodic Discharge
Experiments on Discrete Roughness Element Technology for Swept-Wing Laminar Flow Control
Influence of Continuous Jet at the Lower Surface on Airfoil Aerodynamic Performance
Study of Rotating Menisci in a Generic Propellant-Management Device
Geometric Representation of Flow Features Using the Medial Axis for Mesh Generation
Hypersonic Heat Flux Reconstruction with Distributed Temperature Sensors
Structured and Unstructured Simulations for the Third AIAA Sonic Boom Prediction Workshop
Experimental Analysis of Implementing Roughness on NACA 0018 Airfoil
Polynomial Guidance Law for Dual-Seeker Interceptors
Aerothermodynamic Ground Tests in Support of the Boundary Layer Transition Flight Experiment