Assessment of Transition Modeling Capability in OVERFLOW with Emphasis on Swept-Wing Configurations
Tests of the NACA 65 sub 3 -018 Airfoil Section with Boundary-Layer control by Suction
An Introductory Description of a Hodograph Method for Transonic Shock-Free Aerofoil Design
Six Degree of Freedom Flight Dynamic Model of a MK-82 Store
Higher–Order Aerodynamic Computations Using an Edge Based Finite Volume Scheme
Flight Measurements of Internal Cockpit Pressures in Several Fighter- Type Airplanes
Lifting-Line Theory of Swept Wings Based on the Full Potential Theory
A Wind-Tunnel Investigation of a 7-Foot- Diameter Ducted Propeller
Assessment of Store Control Surface Effectiveness in a Non-Uniform Aircraft Flow Field
Investigation of Plume Induced Separation on a Full-Size Missile at Supersonic Velocities
Study of Flows Over Highly-Swept Wings Designed for Manoeuvre at Supersonic Speeds
Infrared and Phase-Change Paint Measurements of Heat-Transfer on the Space Shuttle Orbiter
Progress in Transition Modelling (Progres dans la Modelisation de la Transition). Special Course
Laser Velocimetry Measurements of Oscillating Airfoil Dynamic Stall Flow Field
Injection, Atomization, Ignition and Combustion of Liquid Fuels in High-Speed Air Streams
Digital simulation of a 6-DOF multi-body dispense with body-on-body collision detection