Supersonic wind tunnel nozzles: A selected, annotated bibliography to aid in the development of quiet wind tunnel technology [PDF]
This bibliography, with abstracts, consists of 298 citations arranged in chronological order. The citations were selected to be helpful to persons engaged in the design and development of quiet (low disturbance) nozzles for modern supersonic wind tunnels.
Wolf, Stephen W. D.
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Energy efficient transport technology: Program summary and bibliography [PDF]
The Energy Efficient Transport (EET) Program began in 1976 as an element of the NASA Aircraft Energy Efficiency (ACEE) Program. The EET Program and the results of various applications of advanced aerodynamics and active controls technology (ACT) as ...
Bartlett, D. W. +2 more
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Numerical study of probe parameters on performance of a transonic axial compressor. [PDF]
PLoS One, 2021 Islam A, Ma H.
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Two-measured variable method for wall interference assessment/correction [PDF]
An iterative method for wall interference assessment and/or correction is presented for transonic flow conditions in wind tunnels equipped with two component velocity measurements on a single interface.
Lo, C. F., Sickles, W. L.
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Aeronautical engineering: A continuing bibliography, supplement 122 [PDF]
This bibliography lists 303 reports, articles, and other documents introduced into the NASA scientific and technical information system in April ...
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Development and Prospect of Smart Materials and Structures for Aerospace Sensing Systems and Applications. [PDF]
Sensors (Basel), 2023 Wang W, Xiang Y, Yu J, Yang L.
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Low-disturbance wind tunnels [PDF]
During the past years, there was an extensive program under way at the Langley Research Center to upgrade the flow quality in several of the large wind tunnels. This effort has resulted in significant improvements in flow quality in these tunnels and has
Applin, Z. T. +3 more
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An experimental investigation of internal area ruling for transonic and supersonic channel flow [PDF]
A simulated transonic rotor channel model was examined experimentally to verify the flow physics of internal area ruling. Pressure measurements were performed in the high speed wind tunnel at transonic speeds with Mach 1.5 and Mach 2 nozzle blocks to get
Rizvi, G. +2 more
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A critical assessment of wind tunnel results for the NACA 0012 airfoil [PDF]
A large body of experimental results, obtained in more than 40 wind tunnels on a single, well-known two-dimensional configuration, has been critically examined and correlated.
Mccroskey, W. J.
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Application of the techniques for evaluating the acoustic sources of background noise in wind tunnel facilities [PDF]
Techniques for evaluating acoustic sources of background noise in wind ...
Boone, J. R., Mc Canless, G. F., Jr.
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