1.

Record Nr.

UNINA9910706120203321

Autore

Campbell Bryan A.

Titolo

Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration / / Bryan A. Campbell [and three others]

Pubbl/distr/stampa

Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999

Descrizione fisica

1 online resource (103 pages) : illustrations

Collana

NASA/TM ; ; 1999-209701

Soggetti

Subsonic wind tunnels

Leading edge flaps

Vortices

Supersonic transports

Aerodynamic configurations

Separated flow

Lingua di pubblicazione

Inglese

Formato

Materiale a stampa

Livello bibliografico

Monografia

Note generali

"December 1999."

"Performing organization: NASA Langley Research Center"--Report documentation page.

Nota di bibliografia

Includes bibliographical references (pages 102-103 ).