NASA NTRS · 19740000206
Computer program for steamtube curvature analysis: Analytical method
Abstract
Program provides design information for low-drag, high-drag-divergence, Mach number isolated nacelles suitable for use with advanced high-bypass-ratio, turbofan engines. One element is development of method to predict inviscid pressure distribution and flow field about arbitrary axisymmetric ducted body at transonic speeds.
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Ferguson, D. R., Heck, P. H., Keith, J. S., Lahti, D. J., Merkle, C. L.. 1974-11-01. Computer program for steamtube curvature analysis: Analytical method. https://ntrs.nasa.gov/citations/19740000206
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