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The Boll-Weevil Problem.

Description: Describes the characteristics of the boll weevil, the damage it causes to cotton crops of the southeastern United States, and methods of control.
Date: June 1923
Creator: Hunter, W. D. (Walter David), 1875-1925 & Coad, B. R.
Item Type: Refine your search to only Book
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Trembles.

Description: Describes the trembles, a milk sickness which afflicts cows; includes information regarding causes, transmission to uninfected animals, remedies, and prevention.
Date: June 1929
Creator: Marsh, C. Dwight (Charles Dwight)
Item Type: Refine your search to only Book
open access

Observations on the Method of Determining the Velocity of Airships

Description: To obtain the absolute velocity of an airship by knowing the speed at which two routes are covered, we have only to determine the geographical direction of the routes which we locate from a map, and the angles of routes as given by the compass, after correcting for the variation (the algebraical sum of the local magnetic declination and the deviation).
Date: June 1921
Creator: Volterra, Vito
Item Type: Refine your search to only Report
open access

The Dynamometer Hub and the Flywheel of the Engine

Description: Report presenting a description of the interaction between the dynamometer hub and the flywheel of the engine in aircraft. The negative rotary moments in propellers generally allow for the cessation of one cylinder without any lifting on the part of the propeller, and without depriving the engine of its flywheel.
Date: June 1921
Creator: Everling, E.
Item Type: Refine your search to only Report
open access

The development of German Army airplanes during the war

Description: From Summary: "The author, who was a captain of the Reserves in the Technical Department of the Aviation Division (Board of Airplane Experts) during the war, shows what means were taken for the creation of new airplane types and what tests were employed for trying out their flying properties, capacities and structural reliability. The principal representative types of each of the classes of airplanes are described and the characteristics of the important structural parts are discussed. Data reg… more
Date: June 1921
Creator: Hoff, Wilhelm
Item Type: Refine your search to only Report
open access

Absolute Coefficients and the Graphical Representation of Aerofoil Characteristics

Description: It is argued that there should be an agreement as to what conventions to use in determining absolute coefficients used in aeronautics and in how to plot those coefficients. Of particular importance are the absolute coefficients of lift and drag. The author argues for the use of the German method over the kind in common use in the United States and England, and for the Continental over the usual American and British method of graphically representing the characteristics of an airfoil.
Date: June 1921
Creator: Munk, Max
Item Type: Refine your search to only Report
open access

Notes on the standard atmosphere

Description: From Summary: "This report contains the derivation of a series of relations between temperature, pressure, density, and altitude in a standard atmosphere which assumes a uniform decrease of temperature with altitude. The equations are collected and given with proper constants in both metric and English units for the temperature gradient adopted by the National Advisory Committee for Aeronautics. A table of values of temperature pressure and density at various altitudes in this standard atmosphe… more
Date: June 1922
Creator: Diehl, Walter S.
Item Type: Refine your search to only Report
open access

Simple formula for estimating airplane ceilings

Description: From Summary: "The aeronautical engineer often has occasion to estimate the absolute ceiling of an airplane for which a detailed performance calculation is out of the question. In such cases it is customary to use either empirical performance charts or formulae. The performance charts given in several of the recent works on aeronautics are satisfactory so long as the airplane under consideration does not depart too far from the average in its characteristics. The formulae, with one exception, a… more
Date: June 1922
Creator: Diehl, Walter S.
Item Type: Refine your search to only Report
open access

On the Distribution of Lift Along the Span of an Airfoil With Displaced Ailerons

Description: "The effect of an aileron displacement on the distribution of the lift along the span is computed for an elliptic wing of aspect ratio 6 for three conditions. The lift distribution caused by the aileron displacement is uniform and extends normally beyond the inner end of the ailerons. Hence, the displacement of an aileron with constant chord length may bring about passing the stalling point of the adjacent wing sections, if these were near this point before" (p. 1).
Date: June 1924
Creator: Munk, Max M.
Item Type: Refine your search to only Report
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