Feasibility and benefits of laminar flow control on supersonic cruise airplanes /
Saved in:
Author / Creator: | Powell, A. G. |
---|---|
Imprint: | Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] |
Description: | 1 volume. |
Language: | English |
Series: | NASA contractor report ; 181817 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. |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/7732544 |