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  • Fluid Mechanics and Thermodynamics  (2)
  • Baikal_1828; BAIKAL_8706; Barents Sea; Bay of Finland; BUCC99_13; Buccaneer; Buccaneer_1899; CHA-285; Challenger1872; Deposit type; DEPTH, sediment/rock; Description; Event label; Grab; GRAB; H.M.S. Challenger (1872); Identification; Kara Sea; Lake Baikal, Russia; LOMO37_1; Lomonosov; Lomonossov1931; NERP30_23; Nerpa; Nerpa_1930; NOAA and MMS Marine Minerals Geochemical Database; NOAA-MMS; Pacific Ocean; PERS26_425; Persey; Persey_1926; Position; Radium; Size; TRALS21_10; Tralshchik; Tralshchik_1921; Visual description; White Sea  (1)
  • Deposit type; DEPTH, sediment/rock; Description; Dredge; DRG; Event label; Identification; Kara Sea; Lake_Uksh_K; Lake Uksh, Karelia, Russia; NOAA and MMS Marine Minerals Geochemical Database; NOAA-MMS; Position; Sedov (1909); Sedov-1934; SEDOV34_74; Size; Substrate type; Visual description  (1)
  • 1940-1944  (1)
  • 1935-1939  (3)
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  • 1
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    Unknown
    PANGAEA
    In:  Supplement to: Kurbatov, L M (1937): On the radioactivity of bottom sediments. American Journal of Science, s5-33(194), 147-153, https://doi.org/10.2475/ajs.s5-33.194.147
    Publication Date: 2023-08-28
    Description: At the date of publication the radioactivity of bottom sediments had only been published by a few authors. The radioactivity of selected characteristic ferro-manganese formations samples taken from different seas and lakes has been determined. This investigations covers nine seas and lakes of the U.S.S.R., and for comparison, two manganese concretions from the Pacific.
    Keywords: Baikal_1828; BAIKAL_8706; Barents Sea; Bay of Finland; BUCC99_13; Buccaneer; Buccaneer_1899; CHA-285; Challenger1872; Deposit type; DEPTH, sediment/rock; Description; Event label; Grab; GRAB; H.M.S. Challenger (1872); Identification; Kara Sea; Lake Baikal, Russia; LOMO37_1; Lomonosov; Lomonossov1931; NERP30_23; Nerpa; Nerpa_1930; NOAA and MMS Marine Minerals Geochemical Database; NOAA-MMS; Pacific Ocean; PERS26_425; Persey; Persey_1926; Position; Radium; Size; TRALS21_10; Tralshchik; Tralshchik_1921; Visual description; White Sea
    Type: Dataset
    Format: text/tab-separated-values, 48 data points
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  • 2
    Publication Date: 2023-08-28
    Keywords: Deposit type; DEPTH, sediment/rock; Description; Dredge; DRG; Event label; Identification; Kara Sea; Lake_Uksh_K; Lake Uksh, Karelia, Russia; NOAA and MMS Marine Minerals Geochemical Database; NOAA-MMS; Position; Sedov (1909); Sedov-1934; SEDOV34_74; Size; Substrate type; Visual description
    Type: Dataset
    Format: text/tab-separated-values, 11 data points
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  • 3
    Publication Date: 2019-07-13
    Description: Problems of hydraulic flow resistance and heat transfer for streams with velocities comparable with acoustic have present great importance for various fields of technical science. Especially, they have great importance for the field of heat transfer in designing and constructing boilers.of the "Velox" type. In this article a description of experiments and their results as regards definition of the laws of heat transfer in differential form for high velocity air streams inside smooth tubes are given.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: NACA-TM-1054 , Journal of Technical Physics; 9; 9; 808-818
    Format: application/pdf
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  • 4
    Publication Date: 2019-08-26
    Description: The drag and the power cost associated with the changing of the nose of a nacelle from a streamline shape to a conventional N.A.C.A. cowling shape was investigated in the N.A.C.A. 20-foot tunnel. Full-scale propellers and nacelles were used. The increment of drag associated with the change of nose shapes was found to be critically dependent on the afterbody of the nacelle. Two streamline afterbodies were tested. The results fo the tests with the more streamlined afterbody showed that the added drag due to the open-nose cowling was only one-fourth of the drag increase obtained with the other afterbody. The results of this research indicate that the power cost, in excess of that with a streamline nose, of using an N.A.C.A. cowling in front of a well-designed afterbody to enclose a 1,500-horsepower engine in an airplane with a speed of 300 miles per hour amounts to 1.5 percent of the engine power. If the open-nose cowling is credited with 1 percent because it cools the front of the cylinders, the non-useful power cost amounts to only 0.5 percent of the engine power.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: NACA-SR-136
    Format: application/pdf
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