NASA NTRS · 19900003238
Supersonic laminar-flow control
Abstract
Detailed, up to date systems studies of the application of laminar flow control (LFC) to various supersonic missions and/or vehicles, both civilian and military, are not yet available. However, various first order looks at the benefits are summarized. The bottom line is that laminar flow control may allow development of a viable second generation SST. This follows from a combination of reduced fuel, structure, and insulation weight permitting operation at higher altitudes, thereby lowering sonic boom along with improving performance. The long stage lengths associated with the emerging economic importance of the Pacific Basin are creating a serious and renewed requirement for such a vehicle. Supersonic LFC techniques are discussed.
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Bushnell, Dennis M., Malik, Mujeeb R.. 1987-12-01. Supersonic laminar-flow control. https://ntrs.nasa.gov/citations/19900003238
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