Optimum full-scale subsonic wind tunnelThe needs and reasons for performing full-scale subsonic research have been studied. Full-scale wind-tunnel requirements are described; recommended size, airspeed, acoustic capabilities, and flow quality are developed; and data-acquisition systems, productivity, automation, and some cost elements are discussed. It is proposed that the optimum full-scale, subsonic wind tunnel be large enough to accommodate aerodynamic and acoustic investigations on most advanced aircraft, which exhibit complex engine/lifting-surface flow-field interactions, including advanced rotorcraft.
Document ID
19950028562
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mort, K. W. (NASA Ames Research Center Moffett Field, CA, United States)
Soderman, P. T. (NASA Ames Research Center Moffett Field, CA, United States)
Meyn, Larry A. (NASA Ames Research Center Moffett Field, CA, United States)