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Author
Powell, A. G.
Title
Feasibility and benefits of laminar flow control on supersonic cruise airplanes [electronic resource] / A.G. Powell, S. Agrawal, T. R. Lacey.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
Connect to
Connect to https://permanent.fdlp.gov/LPS113610/LPS113610/ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890017470_1989017470.pdf
Copies
Location
Call No.
OPAC Message
Status
Axe Federal Documents Online
NAS 1.26:181817
---
Available
Description
1 v.
Series
NASA contractor report ; 181817
NASA contractor report ; NASA CR-181817.
System Details
Mode of access via the NTRS web site.
Note
Title from title screen (viewed Jun. 9, 2009)
Subject
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.
Added Author
Agrawal, S.
Lacey, T. R.
Langley Research Center.
Other Form:
Powell, A. G. Feasibility and benefits of laminar flow control on supersonic cruise airplanes. 1 v. (OCoLC)384139602
Gpo Item No.
0830-H-14 (online)
Sudoc No.
NAS 1.26:181817
Available items only
