Static and unsteady pressure measurements on a 50 degree clipped delta wing at M = 0.9Static and unsteady pressures were measured on a 50.45 degree clipped delta wing in the Langley Transonic Dynamics Tunnel with Freon as the test medium. Data taken at M = 0.9 is presented for static and oscillatory deflections of the trailing edge control surface and for the wing in pitch. Comparisons of the static measured data are made with results computed using the Bailey-Ballhaus small disturbance code.
Document ID
19820046618
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hess, R. W. (NASA Langley Research Center Hampton, VA, United States)
Wynne, E. C. (NASA Langley Research Center Hampton, VA, United States)
Cazier, F. W. (NASA Langley Research Center Loads and Aeroelasticity Div., Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 82-0686
Meeting Information
Meeting: In: Structures, Structural Dynamics and Materials Conference