Path: ACPro/Atmosphere
% Hypersonic sonic boom based on drag. -------------------------------------------------------------------------- Form: [dP, i, t] = SonicBoomHypersonic( drag, m, h, atmData ) -------------------------------------------------------------------------- ------- Inputs ------- drag (1,1) Drag force (N) m (1,1) Mach number h (1,:) Altitude (km) atmData (:,6) Atmospheric data for StdAtm ------- Outputs ------- pG (1,:) N wave overpressure (N) i (1,:) Positive Phase Impulse (N/s) t (3,:) Duration (s) -------------------------------------------------------------------------- Reference: Plotkin, K.J., "Review of Sonic Boom Theory," AIAA-89=-1105, 1989. --------------------------------------------------------------------------
AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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