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Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, Ericksen, Wilhelm S., March, H. W., Smith, C. B., and Boller, Kenneth H.
Abstract:: Information reviewed and reaffirmed April 1961. Previous report dated November 1949.
Resource Type:: Technical Report
Full Text:: of the solution of 1.4.2 is [A 1 Binh vy + A2 sinh vy + B 1 cosh vy T: liX + B 2 cosh Ty] sin

Creator:: Boller, Kenneth H. and Forest Products Laboratory (U.S.)
Abstract:: This report is one of a series issued in cooperation with the ANC-17 Panel on Plastics for Aircraft of the Departments of the Air Force, Navy, and Commerce. Information reviewed and reaffirmed 1965. Original report issued June 1957.
Resource Type:: Technical Report
Full Text:: and time. The strain, e t , at any time, t, may be expressed as E t = e' sinh cr/ cre + to m' sinh o

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, Ericksen, Wilhelm S., Kommers, William J., and Forest Products Laboratory (U.S.)
Abstract:: Supplementary mathematical analysis and comparison with the results of tests. This report is one of a series issued in cooperation with the Army-Navy-Civil Committee on Aircraft Design Criteria under the supervision of the Aeronautical Board.
Resource Type:: Technical Report
Full Text:: Pillila +1 sink a d - sinh a (b + d) _1 cosh a (a + b) -, ..... elf L -.-- - 2 2 - ba3 cosh

Creator:: Forest Products Laboratory (U.S.) and Boller, Kenneth H.
Abstract:: Information reviewed and reaffirmed 1965. Revised September 1958.
Resource Type:: Technical Report
Full Text:: data also showed that the tensile strains may be represented by the relationship, E = E O ' sinh olo-e

Creator:: Youngquist, W. G., Kuenzi, Edward W., and Forest Products Laboratory (U.S.)
Abstract:: This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on Aircraft Design Criteria under the supervision of the Aircraft Committee of the Munitions Board. Information reviewed and reaffirmed 1960. Original report issued March 1955.
Resource Type:: Technical Report
Full Text:: formula 1 results in exponential functions which can be written as hyperbolic functions, thus: sinh a(r

Creator:: Forest Products Laboratory (U.S.) and Boller, Kenneth H.
Resource Type:: Technical Report
Full Text:: sinh a/ae + m' to sinh aiam, where e is total strain in inches per inch, a is applied stress level in

Creator:: Forest Products Laboratory (U.S.)
Abstract:: Originally prepared in 1944. Information reviewed and reaffirmed 1962.
Resource Type:: Technical Report
Full Text:: 2 = - cosh 4 f _jcosh2 (I) - 1 = - cosh (I) f sinh st• e - e -4) = - e4) or -e -4 2 2 -For

Creator:: Youngquist, W. G., Kuenzi, Edward W., and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed in 1960.
Resource Type:: Technical Report
Full Text:: , a r - bl+ ra- sinhpLt a - 1.1 \ ar:To sinh a(a - b) (2) and the formula for the facing stress at

Creator:: Forest Products Laboratory (U.S.) and James, William L.
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Composite Construction for Flight Vehicles of the Departments of the Air Force, Navy, and Commerce.
Resource Type:: Technical Report
Full Text:: Yo (6) M = A sinh x + B cosh x + L 2 1 sin Tr x + Tr D The bending moment vanishes at x = 0

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