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  • Other Sources  (12)
  • Seismology  (4)
  • Witterung  (4)
  • Aircraft Design, Testing and Performance  (3)
  • Earth model, also for more shallow analyses !  (2)
  • BIOSCIENCES
  • Industrial Chemistry
  • Inorganic Chemistry
  • 1970-1974
  • 1950-1954
  • 1930-1934  (12)
  • 1920-1924
  • 1933  (12)
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  • 1970-1974
  • 1950-1954
  • 1930-1934  (12)
  • 1920-1924
Year
  • 1
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    In:  Geologische Rundschau, Milano, Gustav Fischer, vol. 24, no. 3, pp. 227-239, pp. L24306, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1933
    Keywords: Seismology ; Hypocentral depth ; Seismicity
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  • 2
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    In:  Gerlands Beiträge zur Geophysik, Milano, Gustav Fischer, vol. 40, no. 3, pp. 97-98, pp. L24306, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1933
    Keywords: Seismology ; P-waves ; CRUST
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  • 3
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    In:  Gerlands Beiträge zur Geophysik, Milano, Gustav Fischer, vol. 40, no. 3, pp. 380-389, pp. L24306, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1933
    Keywords: mathematics ; geometry ; Seismology
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  • 4
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    In:  Bull. Geol. Soc. Am., Milano, Gustav Fischer, vol. 44, no. 3, pp. 170-171, pp. L24306, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1933
    Keywords: CRUST ; Earth model, also for more shallow analyses ! ; Seismology ; Velocity depth profile
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  • 5
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    Gustav Fischer
    In:  Professional Paper, Handwörterbuch der Naturwissenschaften Bd. 3, Jena, Gustav Fischer, vol. 3, no. VIIa, pp. 762-774, (ISBN: 3-540-23712-7)
    Publication Date: 1933
    Keywords: Handbook of geophysics ; Earth model, also for more shallow analyses !
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  • 6
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    In:  Virchows Archiv für Pathologische Anatomie und Physiologie und für Klinische Medizin, v291 n1-2, 237-259
    Publication Date: 1933
    Description: statistische Bearbeitung von über 16.000 Berliner Sektionsfällen, Vergleich der täglichen Sterbeziffer mit der Wetterlage KATASTER-BESCHREIBUNG: Zunahme der Mortalität an Kaltfront- und Warmfronttagen KATASTER-DETAIL:
    Keywords: Berlin ; 1926-1928 ; Umweltmedizin ; Witterung
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  • 7
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    In:  Vortrag, Schr. Königsberg. gel. Ges., Naturwiss. Kl., 10 H.6) Max Niemeyer, Halle a. S.:16
    Publication Date: 1933
    Description: Untersuchungen über den Einfluss klimatischer Wachstumsfaktoren auf den Ertrag KATASTER-BESCHREIBUNG: Einfluss der Witterung (Temperatur, Niederschlag, Sonnenschein) auf den Ertrag KATASTER-DETAIL: Delta Luftdruck +, dann Erträge +; Delta O2-Gehalt (Luft) = 15 %, dann Ertrag = max; Delta CO2-Gehalt (Luft) = 0.03 %, dann Ertrag = max; Delta Lichtintensität - und Delta CO2-Gehalt +, dann Ertrag +; Delta T Boden, Vegetationszeit) + : Tmit 〉 5 °C, dann Ertrag; Delta Nied +, dann Ertrag +;
    Keywords: Königsberg, Preußen ; 1931-1932 ; Boden ; Ertrag ; Niederschlag ; Temperatur ; Wind ; Witterung ; Sonnenscheindauer
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  • 8
    Publication Date: 1933
    Description: Korrelation zwischen Junitemperaturen und Hafererträgen Regressionsgleichung (Temperaturzunahme bedingt Ertragsrückgang) KATASTER-BESCHREIBUNG: Einfluss der Junitemperatur auf die Haferernte KATASTER-DETAIL: Delta T (Juni) +, dann Erträge --; Änderungen um +1°C, dann Verminderung der Erträge um ~2,1 Zentner; Änderungen um +5°C, dann Verminderung der Erträge um 10 Zentner pro 1 ha
    Keywords: Niederbayern und Oberösterreich ; 1885-1925 ; Ertrag ; Hafer ; Korrelationsmethode ; Niederschlag ; Temperatur ; Witterung
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  • 9
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    In:  Anzeig. Schädlingskunde 9; p.29-34
    Publication Date: 1933
    Description: Der Autor beschreibt Beobachtungen über verschiedene schädigende und nicht schädigende Insekten im Acker- und Obstbau, sowie der Forstwirtschaft und versucht ihre Ursachen im Wetter des Jahres 1932 zu finden. KATASTER-BESCHREIBUNG: KATASTER-DETAIL:
    Keywords: Mecklenburg-Vorpommern ; 1932 ; Niederschlag ; Pflanzenschädling ; Temperatur ; Trockenheit ; Witterung
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  • 10
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    In:  CASI
    Publication Date: 2019-07-12
    Description: Investigations with a view to increasing the lift coefficient of a wing, without greatly increasing the C(sub x min), are chiefly related to the important question of the maximum speed range.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA Misc. Paper No. 37
    Format: application/pdf
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  • 11
    Publication Date: 2019-08-13
    Description: This note discusses the limitations of the conventional tank test of a seaplane model. The advantages of a complete test, giving the characteristics of the model at all speeds, loads, and trim angles in the useful range are pointed out. The data on N.A.C.A. Model No.11, obtained from a complete test, are presented and discussed. The results are analyzed to determine the best trim angle for each speed and load. The data for the best angles are reduced to non-dimensional form for ease of comparison and application. A practical problem using the characteristics of model no.11 is presented to show the method of calculating the take-off time and run of a seaplane from these data.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-TN-464
    Format: application/pdf
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  • 12
    Publication Date: 2019-07-12
    Description: Since the recent more or less extensive adoption of high-lift flaps on airplane wings, the problem of providing satisfactory lateral control without sacrificing a part of the span of the flaps has become one of some importance. The difficulties have been largely a matter of obtaining satisfactory rolling moments with a smoothly graduated action, together with sufficiently small control forces throughout the entire speed range. As part of an investigation including several different lateral-control arrangements to be used with split flaps, the tests reported in this paper were made on one arrangement in which conventional ailerons of narrow chord are used, and a split flap is retracted into the under surface of th wing forward of th ailerons. When the flap is retracted, the arrangement is as sketched in figure 1(a). If a simple form of split flap were used, hinged at its forward edge, the appearance when deflected would be as shown in figure 1(b). The flap if deflected with its leading edge remaining in this forward position would give somewhat less than three fourths of the lift increase of the same flap in the usual rear position. (See reference 1.). If, as shown in figure 1(c), the split flap ahead of th aileron is moved to the rear as the trailing=edge portion is deflected downward, a double advantage is obtained. The deflected flap can be located in the most effective region for high lift (reference 1), and the force required to deflect the flap is reduced. This is the arrangement used in the present tests.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-SR-14
    Format: application/pdf
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