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- W2040061733 abstract "This paper presents and discusses trends in nose shock overpressure generated by two conceptual Mach 2.0 configurations. One configuration was designed for high aerodynamic efficiency, while the other was designed to produce a low boom, shaped-overpressure signature. Aerodynamic lift, sonic boom minimization, and Mach-sliced/area-rule codes were used to analyze and compute the sonic boom characteristics of both configurations with respect to cruise Mach number, weight, and altitude. The influence of these parameters on the overpressure and the overpressure trends are discussed and conclusions are given." @default.
- W2040061733 created "2016-06-24" @default.
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- W2040061733 date "1990-01-08" @default.
- W2040061733 modified "2023-09-26" @default.
- W2040061733 title "A study of sonic boom overpressure trends with respect to weight, altitude, Mach number, and vehicle shaping" @default.
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- W2040061733 doi "https://doi.org/10.2514/6.1990-367" @default.
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