1963•AIAA JournalRequires access

SOLUTION OF THE INCOMPRESSIBLE LAMINAR BOUNDARY-LAYER EQUATIONS

A. M. O. Smith, Darwin W. Clutter

Abstract

AD-266 2719 3 AD-266 272Div. 3, 1U (TIPTW/JRG) OTS price $2.60 Emerson Electric Mfg. Co., St. Louis, Mo. STRUCTURAL TEST UNDER LABORATORY CONDITIONS FOR THE AERO 5A-1 FLARE LAUNCHER, AIRBORNE. 29 Sep 61, 25p. incl. illus. tables (Rept. no. 1228) (Subcontract to Universal Match Corp., St. Louis, Mo.; Contract NOw 61-0514-c) Uncla sified repor SCRIPTORS: (*Aircraft flares, *Pyrotechnic ejectors, Structures, Tests.) Identifiers: Aero 5A-1 flare launcher. S TRUC URAL TESTS OF TH A ro 5A-1 flare launcher were successfully completed. N O PERMAN NT DEFORM ION WAS NOTED AT LIMIT LOADS AND NO FAILURES OCCURRED. (Author)

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Key concepts: Laminar flow, Boundary layer, Compressibility, Mechanics, Blasius boundary layer, Boundary layer thickness, Materials science, Physics