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Creator:: Forest Products Laboratory (U.S.), Smith, C. B., Ringelstetter, L. A., and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: Information reviewed and reaffirmed 1960. Original report dated 1947.
Resource Type:: Technical Report
Full Text:: and the panel without a stiffene r buckles with no nodal lines . k (n + 1)n= if the loaded edges are

Creator:: Forest Products Laboratory (U.S.), Heebink, T. B. (Thomas Bruce), 1914-, March, H. W., and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: Information reviewed and reaffirmed March 1956. Original report published in 1946.
Resource Type:: Technical Report
Full Text:: a=1k +fk2. 31 k = E/^1-37Eb _ o-TLEL 2P-LT '5tTLib The plotted points in figure 11 scatter

Creator:: March, H. 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 1958. Original report issued September 1952.
Resource Type:: Technical Report
Full Text:: Consequently, (6) where K is a constant that will be 'called the stiffness of the sandwich panel in shear

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Kommers, William J.
Abstract:: Information reviewed and reaffirmed 1958. Original report issued June 1952.
Resource Type:: Technical Report
Full Text:: convenient use, equation (2) may be written in the form: 2 1 ± r a,94 fe ra.i3 f173 fFa,8cr 1 e where K

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, Kommers, William J., and Forest Products Laboratory (U.S.)
Abstract:: 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:: STRESSES WITI-IIN A RECTANGULAR, HAT SANDWICI-I PANEL SUI3JECTED.TO

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Ringelstetter, L. A.
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 March 1956. Original report issued October 1948.
Resource Type:: Technical Report
Full Text:: plate. K = coefficient in formula D vL h 2 -cr = Kc "Is a = value of the coefficient lie for an

Creator:: Ringelstetter, L. A., Norris, Charles, B. (Charles Brazer), 1894-, and Forest Products Laboratory (U.S.)
Resource Type:: Technical Report
Full Text:: THE EFFECT OF A STIFFENER ON THE MAXIMUM LOAD OF FIAT PLYWOOD

Creator:: Forest Products Laboratory (U.S.) and Kimel, W. R.
Abstract:: Information reviewed and reaffirmed in 1962.
Resource Type:: Technical Report
Full Text:: + W vs .-, cd ;-1 ult U N U N N I 4 0 0 a) + b0 -I- 71 e'l o k) + ---,gCCI (3.) 0 E

Creator:: Forest Products Laboratory (U.S.) and Kimel, W. R.
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Sandwich Construction of the Departments of the Air Force, Navy, and Commerce. Information reviewed and reaffirmed 1962. Original report issued November 1956.
Resource Type:: Technical Report
Full Text:: 3213 i3 2 1 2 2 1 2 Wmn n m rW (1 - —)r 1 + A + W 1-g mn Amn (1 + Amn 2 r) _ rn 2 k (1

Creator:: Forest Products Laboratory (U.S.) and March, H. W.
Abstract:: 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. Information reviewed and reaffirmed August 1955.
Resource Type:: Technical Report
Full Text:: A k --I 1 EILECTS CF SHEAF? DEEOPMATICr1 IN ME CORE OF A FLAT I

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