Comparison of wind tunnel and flyover noise measurements of the YOV-10A STOL aircraft [PDF]
The YOV-10A Research Aircraft was flown to obtain flyover noise data that could be compared to noise data measured in the 40- by 80- foot wind tunnel at NASA Ames Research Center. The flyover noise measurements were made during the early morning hours on
Atencio, A., Jr., Soderman, P. T.
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Transonic Wind Tunnel Test of Three-dimensional Wing
, 1979 Osamu INANO, Haruhiko Arakawa
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Adaptive-wall wind-tunnel research at NASA-Ames Research Center [PDF]
Adaptive wall wind tunnel research is summarized. Small scale two and three dimensional wind tunnel experiments and numerical experiments with a three dimensional adaptive wall simulator are included.
Mendoza, J. P., Schairer, E. T.
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Wind tunnel test on the performance of windbreak and snow fences
, 1985 Katsuaki TAKEDA +3 more
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Comparison of angle of attack measurements for wind tunnel testing [PDF]
, 2001 Thomas C. Jones, John Hoppe
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Rotorcraft research testing in the National Full-Scale Aerodynamics Complex at NASA Ames Research Center [PDF]
The unique capabilities of the National Full-Scale Aerodynamics Complex (NFAC) for testing rotorcraft systems are described. The test facilities include the 40- by 80-Foot Wind Tunnel, the 80- by 120-Foot Wind Tunnel, and the Outdoor Aerodynamic Research
Johnson, W., Smith, C. A., Warmbrodt, W.
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Dataset of the twin floater of amphibian aircraft in wind tunnel test. [PDF]
Data BriefKaryawan +9 more
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An experimental investigation of three dimensional low speed minimum interference wind tunnel for high lift wings [PDF]
As a means to achieve a minimum interference correction wind tunnel, a partially actively controlled test section was experimentally examined. A jet flapped wing with 0.91 m (36 in) span and R = 4.05 was used as a model to create moderately high lift ...
Joppa, R. G., Shindo, S.
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Estimated Manoeuvrability of T. S. Wakashio-maru-I : Wind Tunnel Test and Rudder Open Test
, 1996 Kiyoshi Tachi, Makoto Endo
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