Method for Estimating the Sonic-Boom Characteristics of Lifting Canard-Wing Aircraft Concepts
Application of Sonic-Boom Minimization Concepts in Supersonic Transport Design
Rapid Empirical Method for Estimating the Gross Takeoff Weight of a High Speed Civil Transport
Nacelle Integration to Reduce the Sonic Boom of Aircraft Designed to Cruise at Supersonic Speeds
Design and Analysis of Low Boom Concepts at Langley Research Center