Research Catalog

Details

Additional authors

1. Agrawal, S.
2. Lacey, T. R.
3. Langley Research Center.

Description

1. 1 v.

Series statement

1. NASA contractor report ; 181817

Uniform title

1. NASA contractor report ; NASA CR-181817.

Subject

1. Aerodynamic configurations
2. Boundary layer control
3. Boundary layer stability
4. Feasibility analysis
5. Fighter aircraft
6. Laminar boundary layer
7. Laminar flow
8. Supersonic aircraft
9. Supersonic cruise aircraft research
10. Supersonic transports

Call number

1. GPO Microfiche NAS 1.26:181817

Additional formats (note)

1. 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.

Reproduction (note)

1. Microfiche.

Author

1. Powell, A. G.

Title

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

Imprint

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

Series

1. NASA contractor report ; 181817
2. NASA contractor report ; NASA CR-181817.

Additional formats

1. 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.

Reproduction

1. Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1989. 2 microfiches.

Connect to:

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

Added author

1. Agrawal, S.
2. Lacey, T. R.
3. Langley Research Center.

Other form:

1. Powell, A. G. Feasibility and benefits of laminar flow control on supersonic cruise airplanes. 1 v. (OCoLC)384172382

Gpo item no.

1. 0830-H-14 (MF)
2. 0830-H-14 (online)

Sudoc no.

1. NAS 1.26:181817