Supersonic Laminar-Flow ControlDetailed, 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.
Document ID
19900003238
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Dennis M Bushnell (Langley Research Center Hampton, United States)
Mujeeb R Malik (High Technology Corporation Hampton, Virginia, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1987
Publication Information
Publication: Research in Natural Laminar Flow and Laminar-Flow Control: Part 3
Publisher: National Aeronautics and Space Administration
Subject Category
Aerodynamics
Report/Patent Number
NASA-CP-2487-PT-3
Meeting Information
Meeting: Research in Natural Laminar Flow and Laminar-Flow Control Symposium
Location: Hampton, VA
Country: US
Start Date: March 16, 1987
End Date: March 19, 1987
Sponsors: National Aeronautics and Space Administration