02477cam a2200421Ii 4500103083068MiAaHDL20231207000000.0m d cr bn ---auaua210616s1965 ohua bt f000 0 eng d(MiU)99187887001406381sdr-miu.99187887001406381(OCoLC)1256665203(GWLA)gwla on1256665203TRAALengTRAALMAIND 301.45/46-2:64-194Heinrich, H. G.,author.Dynamic stability of a system consisting of a stable parachute and an unstable load /H.G. Heinrich, L.W. Rust, 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.viii 29 pages :illustrations ;28 cm.texttxtrdacontentunmediatednrdamediavolumencrdacarrierAir Force Flight Dynamics Laboratory (U.S.). Technical report ;AFFDL TR 64-194"May 1965."Includes bibliographical references (page 29)The several equations of motion governing the dynamic stability of a parachute-load system, in which the parachute as well as the load possesses aerodynamic drag and stability characteristics, are established. The general equations are linearized, which process provides satisfactory results for relatively small deflections. A further simplification is accomplished under the assumption of a vertical descent. A numerical example is used to illustrate the application of the analytical methods.Research supported by the United States Air Force Research and Technology Division, and performed by University of Minnesota, Department of Aeronautics and Engineering Mechanics, Minneapolis, Minnesota, under contract no.AF33(657)-11184Mode of access: Internet.Drag (Aerodynamics)Space vehiclesAtmospheric entry.Aerodynamic load.ParachutesAerodynamics.Rust, L. W.,Jr.,author.United States.Air Force.Systems Command.Research and Technology Division,issuing body.Air Force Flight Dynamics Laboratory (U.S.),sponsor.University of Minnesota,sponsor.390150953219343901509532193410308306820231109074255.020231207000000.020231207140605.02024-07-02T17:31:55Z2024-07-02T17:30:02ZSDR-MIUmiuALMAprepare.pl-004-008BKsdr-miu.99187887001406381MiUSDRGWLAmdp.39015095321934MIU99187887001406381MIUGWLA20240702googlemdp.390150953219341965pdbibUS fed doc