Works on Theory of Functions of Complex Variable
Wind Tunnel Tests of 16 Percent Thick Airfoil Section with Spoilers at Different Chordwise Positions
Wind Tunnel Test of a Self-Optimizing Flexible Technology Wing
Wet Double Clutch: Thinking in Systems
Variational Approach to the Problem of the Minimum Induced Drag of Wings
Variational Approaches to Fracture
Using splitter blades to improve suction performance of centrifugal impeller pumps
Unsteady Aerodynamic Analysis of Space Shuttle Vehicles. Part 3: Booster Interference Effects
Two-Dimensional Bifurcated Inlet/Engine Tests Completed in 10- by 10-Foot Supersonic Wind Tunnel