02756cam a2200469Ii 4500102893788MiAaHDL20250726000000.0m d cr bn ---auaua040629s1965 ohua bt f000 0 eng d55756390(MiU)99187625984006381sdr-miu.99187625984006381(OCoLC)1139376281(GWLA)gwla on1139376281LHLengrdaLHLOCLCOOCLCFOCLCQTRAALMAINTL752.H45 1965D 301.45/34-2: 64-125Heinrich, H. G.,author.Stress analysis of a parachute during inflation and at steady state /Helmut G. Heinrich, Lelan R. Jamison, Jr.Wright-Patterson Air Force Base, Ohio :Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force,1965.ix, 46, [2] pages :illustrations, figures ;28 cmtexttxtrdacontentunmediatednrdamediavolumencrdacarrierTechnical documentary report (Air Force Flight Dynamics Laboratory (U.S.)) ;AFFDL-RTD-TDR-64-125"February 1965."Includes bibliograpical references (page 42).The stresses occurring in the cloth of an opening parachute and at steady state are calculated. The method is based on assumed instantaneous and steady state shapes and related pressure distributions. It is general and may be applied to any type and size of canopy built out of solid cloth. The presented analysis is limited to canopies constructed of triangular gores, but can be extended to other gore patterns. A numerical calculation is made for the Solid Flat, Circular Parachute during the opening and at steady state.Air Force Contract No.AF 33(657)-11184, Project No. 6065, Task No. 606503.University of Minnesota, Dept. of Aeronautics and Engineering MechanicsAF33(657)-111846065606503Mode of access: Internet.Strains and stressesAnalysis.Textile chemistry.ParachutesMaterialsAnalysis.ParachutesDeploymentAnalysis.Jamison, Lelan R.,Jr.,author.United States.Air Force.Systems Command,issuing body.Air Force Flight Dynamics Laboratory (U.S.),sponsor.University of Minnesota.Department of Aerospace Engineering and Mechanics,sponsor.Technical Report Archive & Image Library (TRAIL)3901510495657110289378820220802102022.020250726000000.020260306165531.02026-03-07T09:52:43Z2024-08-06T17:30:02ZSDR-MIUmiuALMAprepare.pl-004-009BKsdr-miu.99187625984006381MiUSDRGWLAmdp.39015104956571MIU99187625984006381MIUGWLA20260307googlemdp.390151049565711965pdbibUS fed doc