REFERENCED DOCUMENTS
(2-1) BJORKSTEN, J., ELLIOTT, J. C., and ROTH, R. J.
1952. Foamed Metal Low-Density Core Material for Sandwich
Construction. Wright Air Develop. Center Tech. Rep. 52-51.
(2-2) CADY, W. M., et al
1948. Radar Scanners and Radomes. Mass. Inst. Technol., Radiation Lab. Series, Vol. 26, McGraw-Hill Book Co., N.Y.
(2-3) CAMPAGNA, P. J., PRESTON, H.M., and WAHL, N.E.
1954. Development of Heat-Resistant Foamed-In-Place Dielectric Core Materials for Sandwich Radomes. Wright Air Develop. Center Tech. Rep. 54-249.
(2-4) DOYLE, D. V., and DROW, J. T.
1946. The Elastic Properties of Wood, Young's Moduli, Moduli of Rigidity, and Poisson's Ratios of Mahogany and Khaya. U.S. Forest Prod. Lab. Rep. 1528-C.
(2-5) DOYLE, D. V., DROW, J. T., and McBURNEY, R. S.
1945. The Elastic Properties of Wood--The Young's Moduli,
Moduli of Rigidity, and Poisson's Ratios of Balsa and Quipo. U.S. Forest Prod. Lab. Rep. 1528.
(2-6) EICKNER, H. W.
1957. Weathering of Adhesive-Bonded Lap Joints of Clad Aluminum
Alloy. Wright Air Develop. Center Tech. Rep. 54-447, Part I.
(2-7) EICKNER, K. W.
1955. Weathering of Adhesive-Bonded Lap Joints of Clad Aluminum
Alloy. Wright Air Develop. Center Tech. Rep. 54-447, Part I.
(2-8) FAHEY, D. J., SETTERHOLM, V. C., SEIDL, R. J., and KUENZI, E. W.
1956. Paper Honeycomb Core for Marine Applications. U.S. Forest Prod. Lab. Rep. to BuShips.
(2-9) GOLAND, M., and REISSNER, E.
1944. Stress in Cemented Joints. Journal of Applied Mechanics.
(2-10) HEEBINK, B. G., KOMMERS, W. J., and MOHAUPT, A. A.
1950. Durability of Low-Density Core Materials and Sandwich Panels of the Aircraft Type as Determined by Laboratory Tests and Exposure to the Weather, Part III. U.S. Forest Prod. Lab. Rep. 1573-B.
(2-11) JENKINSON, P. M.
1965. Effect of Core Thickness and Moisture Content on Mechanical Properties of Two Resin-Treated Paper Honeycomb Cores. U.S. Forest Serv. Research Paper FPL 35, Forest Prod. Lab., Madison, Wis.
(2-12) JENKINSON, P. M., FAHEY, D. J., KUTSCHA, D. F., and KUENZI, E. W.
1961. Effect of Core Thickness on Compression Properties of Resin-Treated Paper Honeycomb Core. U.S. Forest Prod. Lab. Rep. SANDIA 2.
(2-13) JENKINSON, P. M., and KUENZI, E. W.
1962. Effect of Core Thickness on Shear Properties of Aluminum Honeycomb Core. U.S. Forest Prod. Lab. Rep. 1886.
(2-14) JENKINSON, P. M., and KUENZI, E. W.
1962. Fatigue Properties of Some Aluminum and Stainless Steel Sandwich Constructions. ASD-TDR-62-1003.
(2-15) JENKINSON, P. M., and KUENZI, E. W.
1957. Mechanical Properties of 422-J Bacfoam Core for Sandwich
Construction. Wright Air Develop. Center Tech. Rep.
57-132. (Astia Doc. No. AD 118249).
(2-16) JENKINSON, P. M., and KUENZI, E. W.
1957. Properties of Alkyd-Isocyanate Foamed-In-Place
Core. Wright Air Develop. Center Tech. Rep. 57-182. (Astia
Doc. No. 155884).
(2-17) KREITH, F.
1960. Principles of Heat Transfer. International Textbook Co., Scranton, Pa.
(2-18) KUENZI, EDWARD W., and STEVENS, GORDON H.
1963. Determination of Mechanical Properties of Adhesives for Use in the Design of Bonded Joints. U. S. Forest Service Research Note FPL-011. Forest Prod. Lab., Madison, Wis.
(2-19) KUENZI, E. W.
1955. Mechanical Properties of Aluminum Honeycomb Cores. U. S. Forest Prod. Lab. Rep. 1849.
(2-20) KUENZI, E. W.
1949. Effect of Elevated Temperatures on the Strengths of Small Specimens of Sandwich Construction of the Aircraft Type--Tests Conducted Immediately After the Test Temperature Was Reached. U.S. Forest Prod. Lab. Rep. 1804.
(2-21) LIBOVE, C., and HUBKA, R. E.
1951. Elastic Constants for Corrugated-Core Sandwich Plates. NACA Tech. Note 2289.
(2-22) McCOWN, J. W., BARRETT, W. F., and NORTON, A. M.
Design and Testing of a Hot Redundant Structures Concept for a Hypersonic Flight Vehicle. Martin-Marietta Corp., Baltimore, Md.
(2-23) NATIONAL DEFENSE RESEARCH COMMITTEE
1951. Tables of Dielectric Materials. Vols. I and II, Lab. for Insulation Res., Mass. Inst. Technol.
(2-24) O'BRIEN, F. R., and OGLESBY, S., JR.
1955. Investigation of Thermal Properties of Plastic Laminates,
Core, and Sandwich Panels. Wright Air Develop. Center Tech. Rep. 54-306, Part 2.
(2-25) SAPOWITH, A. D.
1959. Transverse Shear Stiffness for the Double "V" Corrugated-Core Sandwich Panel. Aero/Space Eng. pp. 53-56, Sept.
(2-26) SETTERHOLM, V. C., HEEBINK, B. G., and KUENZI, E. W.
1955. Durability of Low-Density Sandwich Panels of the Aircraft Type as Determined by Laboratory Tests and Exposure to Weather. U.S. Forest Prod. Lab. Rep. 1573-C.
(2-27) SETTERHOLM, V. C., and KUENZI, E. W.
1956. Effect of Moisture Sorption on Weight and Dimensional Stability of Alkyd-Isocyanate Foam Core. Wright Air Develop. Center Tech. Rep. 56-86.
(2-28) SETTERHOLM, V. C., and KUENZI, E. W.
1956. Performance of Sandwich with Cores of Foamed Silicone and Modified Polyester Resins at Elevated Temperatures and High Humidity. Wright Air Develop. Center Tech. Rep. 56-230. (Astia Doc. No. AD 110421).
(2-29) SETTERHOLM, V. C., EICKNER, H. W., and KUENZI, EDWARD W.
1956. Tensile Strength of Adhesive Bonds in Sandwich with Aluminum Facings and Aluminum Honeycomb Cores. Wright Air Develop Center Tech. Rep. 56-239.
(2-30) SWANN, R. T., and PITTMAN, C. M. 1961. Analysis of Effective Thermal Conductivities of Honeycomb-Core and Corrugated-Core Sandwich Panels. NASA Tech. Note D714.
(2-31) U.S. AIR FORCE-NAVY
1948. Radome Engineering Manual. Air Materiel Command Manual No. 80-4, NAVER 16-45-502.
(2-32) U.S. DEPARTMENT OF DEFENSE
1951. Design of Wood Aircraft Structures. Air Force,
Navy, Commerce Bulletin 18. 2nd ed. Munitions Board Aircraft Comm.
(2-33) U.S. DEPARTMENT OF DEFENSE
1951. Wood Aircraft Inspection and Fabrication. Air Force, Navy, Commerce Bulletin 19. Munitions Board Aircraft Comm.
(2-34) U.S. DEPARTMENT OF DEFENSE
Current Plastics for Flight Vehicles: Part I, Reinforced
Plastics. Military Handbook 17. Armed Forces Supply Support Center. Available from U. S. Gov. Printing Office, Washington, D.C.
(2-35) U.S. DEPARTMENT OF DEFENSE
Current Metallic Materials and Elements for Aerospace
Vehicle Structures. Military Handbook 5. Available from U. S. Gov Printing Office, Washington, D.C.
(2-36) U.S. DEPARTMENT OF DEFENSE
Current Adhesive Bonding, Process and Inspection Requirements for. Military Specification MIL-A-9067.
(2-37) U.S. DEPARTMENT OF DEFENSE
Current Adhesive, Metallic Structural Sandwich Construction. Military Specification MIL-A-25463.
(2-38) U.S. DEPARTMENT OF DEFENSE
Current Core Material, Aluminum, for Sandwich Construction. Military Specification MIL-C-7438.
(2-39) U.S. DEPARTMENT OF DEFENSE
Current Core Material, Plastic Honeycomb, Laminated Glass Fabric Base, for Aircraft Structural Applications. Military Specification MIL-C-8073.
(2-40) U.S. DEPARTMENT OF DEFENSE
Current Core Material, Foamed-In-Place, Urethane Type. Military Specification MIL-C-8087.
(2-41) U.S. DEPARTMENT OF DEFENSE
Current Core Materials, Metallic, Heat-Resistant, for
Structural Sandwich Construction. Military Specification MIL-C-21275.
(2-42) U.S. DEPARTMENT OF DEFENSE
Current Lumber, Hardwood, Mahogany, Aircraft Quality.
Military Specification MIL-L-7970.
(2-43) U.S. DEPARTMENT OF DEFENSE
Current Sandwich Construction, Core Material, Balsa Wood. Military Specification MIL-S-7998.
(2-44) U.S. DEPARTMENT OF DEFENSE
Current Sandwich Construction, Plastic Resin, Glass Fabric Base, Laminated Facings and Urethane Foamed-In-Place Core, for Structural Applications. Military Specification MIL-S-25392.
(2-45) U.S. DEPARTMENT OF DEFENSE
Current Sandwich Construction and Core Materials; General Test Methods. Military Standard MIL-STD-401.
(2-46) U.S. FOREST PRODUCTS LABORATORY, FOREST SERVICE
1955. Wood Handbook. U.S. Dep. Agr., Agr. Handb. 72.
(2-47) U.S. GENERAL SERVICES ADMINISTRATION
Current Adhesives, Heat Resistant, Airframe Structural, Metal-to-Metal. Federal Specification MMM-A-132. Federal Supply Services.
(2-48) VOSS, A. W., and NORRIS, C. B.
1949. Creep Tests of Sandwich Constructions Subjected to Shear at Normal Temperatures. U.S. Forest Prod. Lab. Rep. 1806.
(2-49) WERREN, F.
1952. Shear-Fatigue Properties of Various Sandwich Constructions. U.S. Forest Prod. Lab. Rep. 1837.
(2-50) WIEPKING, C. A., and DOYLE, D. V.
1944. Strength and Related Properties of Balsa and Quipo Woods. U.S. Forest Prod. Lab. Rep. 1511.
(2-51) WILKS, S. S.
1948. Sampling and Its Uncertainties. American Society for Testing Materials, Proceedings Vol. 48.