NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Subsonic and transonic pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfacesA high aspect ratio supercritical wing with oscillating control surfaces is described. The semispan wing model was instrumented with 252 static orifices and 164 in situ dynamic pressure gases for studying the effects of control surface position and sinusoidal motion on steady and unsteady pressures. Data from the present test (this is the second in a series of tests on this model) were obtained in the Langley Transonic Dynamics Tunnel at Mach numbers of 0.60 and 0.78 and are presented in tabular form.
Document ID
19850009695
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sandford, M. C. (NASA Langley Research Center Hampton, VA, United States)
Ricketts, R. H. (NASA Langley Research Center Hampton, VA, United States)
Watson, J. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-83201
L-14831
NAS 1.15:83201
Accession Number
85N18004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available