SOLUTION OF THE INCOMPRESSIBLE LAMINAR BOUNDARY LAYER EQUATIONS

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)

Document Details

Document Type
Technical Report
Publication Date
Jul 29, 1961
Accession Number
AD0266271

Entities

People

  • A.m.o. Smith
  • Darwin W. Clutter

Organizations

  • Douglas

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Airborne
  • Aircraft Flares
  • Aircrafts
  • Boundaries
  • Boundary Layer
  • Buildings And Structures
  • Contracts
  • Equations
  • Flares
  • Laminar Boundary Layer
  • Launchers
  • Layers
  • Mechanical Structure
  • Pyrotechnic Projectors
  • Research Facilities

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Munitions and Ordnance Engineering
  • Snow Cover Descriptors for Reptiles and Their Illustrations.