HSCT design for reduced sonic boom
- Haglund, George T.
- Apr 1, 1992.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- 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.
- Document ID: 19940028965.
Accession ID: 94N33471.
NASA. Langley Research Center, First Annual High-Speed Research Workshop, Part 2; p 703-719.
- No Copyright.
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