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Recommended Experimental Procedures for Evaluation of Abrupt Wing Stall Characteristics
Performance of Advanced Heavy-Lift, High-Speed Rotorcraft Configurations
Performance of Advanced Heavy-Lift, High-Speed Rotorcraft Configurations
Integration of Rotor Aerodynamic Optimization with the Conceptual Design of a Large Civil Tiltrotor
Turbine Bypass Engine: A New Supersonic Cruise Propulsion Concept
Electric Propulsion Concepts Enabled by High Power Systems for Space Exploration
Free-To-Roll Analysis of Abrupt Wing Stall on Military Aircraft at Transonic Speeds
UNO Aviation Monograph Series: The Airline Quality Rating 1997
Hybrid Propulsion Technology Program, Phase 1. Volume 1: Executive Summary
F/A-18C to E Wing Morphing Study for the Abrupt Wing Stall Program
Free Molecule Micro-Resistojet: An Interesting Alternative to Nozzle Expansion