George T. Haglund

发表

Potential for Sonic Boom Reduction of the Boeing HSCT

George T. Haglund, 1999 .

Two HSCT Mach 1.7 low sonic boom designs

George T. Haglund, Steven S. Ogg, 1992 .

Low Sonic Boom Design Activities at Boeing

George T. Haglund, 1999 .

A practical low-boom overpressure signature based on minimum sonic boom theory

R. J. Mack, Robert J. Mack, George T. Haglund, 1992 .

Nacelle and forebody considerations in design for reduced sonic boom

George T. Haglund, 1992 .

Sonic boom loudness study and airplane configuration development

George T. Haglund, Jessica G. Brown, G. Haglund, 1988 .

HSCT designs for reduced sonic boom

George T. Haglund, 1991 .