Research Catalog

Title

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

Author

Powell, A. G.

Publication

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]

Details

Additional Authors

• Agrawal, S.
• Lacey, T. R.
• Langley Research Center.

Description

1 v.

Series Statement

NASA contractor report ; 181817

Uniform Title

NASA contractor report ; NASA CR-181817.

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

Note

• Title from title screen (viewed Jun. 9, 2009).

System Details (note)

• 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.

Call Number

GPO Internet NAS 1.26:181817

OCLC

384172382

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]

Series

NASA contractor report ; 181817

NASA contractor report ; NASA CR-181817.

System Details

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.

Connect to:

http://purl.access.gpo.gov/GPO/LPS113610

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

Research Call Number

GPO Internet NAS 1.26:181817