NASA NTRS ยท 19940028965
HSCT design for reduced sonic boom
Abstract
The topics covered include the following: low sonic boom design perspective; design approach for reduced sonic boom; target sonic boom waveforms; airplane design for reduced sonic boom loudness; design procedure for low sonic boom; wing design and nacelle lift effects; area distributions and F-functions due to volume; fuselage area distributions; low sonic boom design, configuration 3B; sonic boom characteristics; sizing, performance, and noise characteristics; a summary of phase 3 configurations; impact of sonic boom design constraints; and wing loading considerations.
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Haglund, George T.. 1992-04-01. HSCT design for reduced sonic boom. https://ntrs.nasa.gov/citations/19940028965
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