Feasibility and benefits of laminar flow control on supersonic cruise airplanes A.G. Powell, S. Agrawal, T. R. Lacey.

Bibliographic Details
Main Author: Powell, A. G.
Corporate Author: Langley Research Center.
Other Authors: Agrawal, S., Lacey, T. R.
Format: Book Government Document
Language:English
Published: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
Series:NASA contractor report ; NASA CR-181817.
Subjects:
Online Access:CONNECT
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245 1 0 |a Feasibility and benefits of laminar flow control on supersonic cruise airplanes  |h [electronic resource] /  |c A.G. Powell, S. Agrawal, T. R. Lacey. 
260 |a Hampton, Va. :  |b National Aeronautics and Space Administration, Langley Research Center,  |c [1989] 
300 |a 1 v. 
490 1 |a NASA contractor report ;  |v 181817. 
538 |a Mode of access: 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. 
500 |a Title from title screen (viewed Jun. 9, 2009). 
650 7 |a Aerodynamic configurations.  |2 nasat. 
650 7 |a Boundary layer control.  |2 nasat. 
650 7 |a Boundary layer stability.  |2 nasat. 
650 7 |a Feasibility analysis.  |2 nasat. 
650 7 |a Fighter aircraft.  |2 nasat. 
650 7 |a Laminar boundary layer.  |2 nasat. 
650 7 |a Laminar flow.  |2 nasat. 
650 7 |a Supersonic aircraft.  |2 nasat. 
650 7 |a Supersonic cruise aircraft research.  |2 nasat. 
650 7 |a Supersonic transports.  |2 nasat. 
700 1 |a Agrawal, S. 
700 1 |a Lacey, T. R. 
710 2 |a Langley Research Center. 
776 1 |a Powell, A. G.  |t Feasibility and benefits of laminar flow control on supersonic cruise airplanes.  |h 1 v.  |w (OCoLC)384139602. 
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