Feasibility and benefits of laminar flow control on supersonic cruise airplanes /

Bibliographic Details
Main Author:	Powell, A. G.
Corporate Author:	Langley Research Center
Other Authors:	Agrawal, S., Lacey, T. R.
Format:	Government Document Microform Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
Series:	NASA contractor report ; NASA CR-181817.
Subjects:	Aerodynamic configurations. Boundary layer control. Boundary layer stability. Feasibility analysis. Fighter aircraft. Laminar boundary layer. Laminar flow. Supersonic aircraft. Supersonic cruise aircraft research. Supersonic transports.
Online Access:	https://purl.fdlp.gov/GPO/LPS113610

Description
Item Description:	Microform.
Physical Description:	1 volume Also available via Internet from the NTRS web site. Address as of 06/09/09: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890017470%5F1989017470.pdf ; current access is available via PURL.