Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /

Bibliographic Details

Main Author:	Schuster, D. M. (David M.)
Corporate Author:	Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : Hanover, MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), [2001]
Series:	NASA technical memorandum ; 210828.
Subjects:	Transonic wind tunnels. Aerodynamic characteristics. Dynamic pressure. Static pressure. Viscous flow. Wind tunnel tests.
Online Access:	Adobe Acrobat Reader required