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Creator:: Cheng, Shun and Forest Products Laboratory (U.S.)
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:: (1 + 2h 2 Dl (1 - v)Dx + 2Dy Report No. 1874-A -2- Dx Dy D D2 2Dx + (1 - v) Dy am (2m

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 August 1962. Original report dated November 1956.
Resource Type:: Technical Report
Full Text:: defined by a t 3 + (V) 3 F 12 tt't + t' 2 IT (c + t + 2 tt' c 2 IM t + v El D -p.21 EIT D T

Creator:: Ericksen, Wilhelm S. 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. Revised June 1953.
Resource Type:: Technical Report
Full Text:: of equilibrium are derived, Radial forces on facings: TIT (rN r o) - N r-r = 0, (1) d dr

Creator:: Forest Products Laboratory (U.S.) and Kimel, W. R.
Abstract:: Information reviewed and reaffirmed in 1962.
Resource Type:: Technical Report
Full Text:: . Appendix C -- Examples of Integrations 91 4. Appendix D Determinant Elements for Case a = 0, E Finite

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Zahn, John J.
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:: which I+ I (d 1 d d 2 ) T Ex2 1 f 1 f 2 + rid i Sx lidsSy + E z 2 f 1 +f 2 2 ( c += f

Creator:: Werren, Fred and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed 1958 and 1965. Original report issued July 1952.
Resource Type:: Technical Report
Full Text:: , "Aluminum or Fiberglas-laminate Face and Fiberglas Honeycomb Core Sandwich Material," 1948. (4) 1559-D

Creator:: Heebink, Bruce G. 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.
Resource Type:: Technical Report
Full Text:: -texture d cushion, appeared to be simple and practicable, and required a minimum of equipment . The heat

Creator:: 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.
Resource Type:: Technical Report
Full Text:: sandwich and "edgewise direction" used to describe directions of loa d e, to directions that are e core

Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward W.
Abstract:: Information reviewed and reaffirmed 1958. Original report issued November 1951.
Resource Type:: Technical Report
Full Text:: load P h = total sandwich thickness b = width of sandvich bf,fo(h + c) 2 E D = ` 4 (h c) X f 12

Creator:: Forest Products Laboratory (U.S.) and Werren, Fred
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 July 1952.
Resource Type:: Technical Report
Full Text:: facings an d a core of expanded aluminum honeycomb . Repeated tests were made at a ratio of minimum to

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