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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Tables for computing various cases of beam columns

Tables for computing various cases of beam columns

Date: August 1, 1941
Creator: Cassens, J
Description: For a better understanding of these tables, the methods by which the cases are computed are discussed first. The importance of the buckling modules is pointed out.
Contributing Partner: UNT Libraries Government Documents Department
Tables for determining reduction of energy and intensity of X-rays and gamma-rays at various scattering angles in small thickness of matter

Tables for determining reduction of energy and intensity of X-rays and gamma-rays at various scattering angles in small thickness of matter

Date: February 1, 1950
Creator: Allen, G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tables for pressure of air on coming to rest from various speeds

Tables for pressure of air on coming to rest from various speeds

Date: January 1, 1930
Creator: Zahm, A F & Louden, F A
Description: In Technical Report no. 247 of the National Advisory Committee for Aeronautics theoretical formulas are given from which was computed a table for the pressure of air on coming to rest from various speeds, such as those of aircraft and propeller blades. In that report, the table gave incompressible and adiabatic stop pressures of air for even-speed intervals in miles per hour and for some even-speed intervals in knots per hour. Table II of the present report extends the above-mentioned table by including the stop pressures of air for even-speed intervals in miles per hour, feet per-second, knots per hour, kilometers per hour, and meters per second. The pressure values in table II are also more exact than values given in the previous table. To furnish the aeronautical engineer with ready numerical formulas for finding the pressure of air on coming to rest, table I has been derived for the standard values specified below it. This table first presents the theoretical pressure-speed formulas and their working forms in C. G. S. Units as given in NACA Technical Report No. 247, then furnishes additional working formulas for several special units of speed. (author).
Contributing Partner: UNT Libraries Government Documents Department
Tables for the computation of wave drag of arrow wings of arbitrary airfoil section

Tables for the computation of wave drag of arrow wings of arbitrary airfoil section

Date: June 1, 1954
Creator: Grant, Frederick C & Cooper, Morton
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tables for the Computation of Wave Drag of Arrow Wings of Arbitrary Airfoil Section

Tables for the Computation of Wave Drag of Arrow Wings of Arbitrary Airfoil Section

Date: June 1954
Creator: Grant, Fredrick C.
Description: Tables and computing instructions for the rapid evaluation of the wave drag of delta wings and of arrow wings having a ration of the tangent of the trailing-edge sweep angle to the tangent of the leading-edge sweep angle in the range from -1.0 to 0.8. The tables cover a range of both subsonic and supersonic leading edges.
Contributing Partner: UNT Libraries Government Documents Department
Tables for the numerical determination of the Fourier transform of a function of time and the inverse Fourier transform of a function of frequency, with some applications to operational calculus methods

Tables for the numerical determination of the Fourier transform of a function of time and the inverse Fourier transform of a function of frequency, with some applications to operational calculus methods

Date: October 1, 1957
Creator: Huss, Carl R & Donegan, James J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tables of characteristic functions for solving boundary-value problems of the wave equation with application to supersonic interference

Tables of characteristic functions for solving boundary-value problems of the wave equation with application to supersonic interference

Date: February 1, 1957
Creator: Nielsen, Jack N
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tables of Chemical Kinetics : Homogeneous Reactions (Supplementary Tables)

Tables of Chemical Kinetics : Homogeneous Reactions (Supplementary Tables)

Date: September 15, 1961
Creator: United States. Bureau of Standards.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tables of Chemical Kinetics : Homogeneous Reactions (Supplementary Tables)

Tables of Chemical Kinetics : Homogeneous Reactions (Supplementary Tables)

Date: July 1, 1964
Creator: United States. Bureau of Standards.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tables of coefficients for the analysis of stresses about cutouts in circular semimonocoque cylinders with flexible rings

Tables of coefficients for the analysis of stresses about cutouts in circular semimonocoque cylinders with flexible rings

Date: July 1, 1955
Creator: Mccomb, Harvey G , Jr & Low, Emmet F , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department