113 research outputs found
Power-Off Tests of the Northrop N9M-2 Tailless Airplane in the 40- by 80-foot Wind Tunnel
No abstract availabl
Tests of an Attack-Type Airplane in the Ames 40- by 80-Foot Wind Tunnel to Improve the High-Speed Maneuvering Control-Force Characteristics
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Aerodynamic Characteristics in Sideslip of a Large-scale Model Having a 63 Degree Swept-back Vertical Tail
A base for biodiversity data
For the last 20 years, the Cook Islands Natural Heritage Trust has been collecting the details of the country's fauna and flora in one multimedia database
Biodiversité en base de données
Voilà 20 ans que Cook Islands Natural Heritage Trust recueille des données sur la faune et la flore insulaires et les consigne dans une base de données multimédi
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Investigation of a Large-scale Model at Low Speed
Effects of Boundary-layer Control on the Longitudinal Characteristics of a 45 Degrees Swept-forward Wing-fuselage Combination
The Effects of Boundary-layer Control on the Longitudinal Characteristics of a Swept-back Wing Using Suction Through Streamwise Slots in the Outboard Portion of the Wing
An Investigation of the Low-speed Stability and Control Characteristics of Swept-forward and Swept-back Wing in the Ames 40- by 80-foot Wind Tunnel
An investigation has been made at large scale of the characteristics of highly swept wings. Data were obtained at several angles of sideslip on wings having angles of sweep of plus or minus 45 degrees, plus or minus 30 degrees, and 0 degrees. The airfoil sections of the wings varied from approximately NACA 0015 at the root to NACA 23009 at the tip. Each wing was investigated with flaps under flection, partial-span split flaps deflected 60 degrees, full-span split flaps defected 60 degrees and split-flap-type ailerons deflected plus or minus 15 degrees. Values of maximum lift were obtained at Reynolds numbers raging from 5.7 to 9.2 times 10 to the 6th power. In this report the summarized results are compared with the predictions made by use of the simplified theory for the effect of sweep and with existing small-scale data. The basic wind-tunnel results from which these summary data were taken are included in an appendix. The primary problems accompanying the use of weep as revealed by this investigation are the loss in maximum lift, the high effective dihedral, and the sharp reduction in lateral-control effectiveness. In general, simple theory enables good predictions to be made of the gross effects of sweep but further refinements are necessary to obtain the accuracy required for design purposes. In cases where comparisons can be made, the indications are that, as sweep increases, scale effects diminish and large-scale results approach small-scale results
A contribution to knowledge of Dermestidae (Coleoptera) from Cook Islands
The following species are newly recorded from the Cook Islands: Anthrenus (Anthrenus) oceanicus Fauvel, 1903, Evorinea iota (Arrow, 1915), Orphinus (Orphinus) fulvipes (Guérin-Méneville, 1838), Dermestes (Dermestinus) carnivorus Fabricius, 1775
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