02134oam 2200577I 450 991070780570332120170110161520.0(CKB)5470000002468506(OCoLC)755080648(EXLCZ)99547000000246850620110929j198712 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSemiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane /Bandu N. Pamadi, Lawrence W. Taylor[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Division,December 1987.1 online resource (vii, 80 pages) illustrationsNASA technical memorandum ;4009"December 1987" Report documentation page."Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 18-19).Spin (Aerodynamics)fastAerodynamic coefficientsnasatAerodynamic forcesnasatCentrifugal forcenasatEstimatesnasatRotating bodiesnasatSpin (Aerodynamics)Aerodynamic coefficients.Aerodynamic forces.Centrifugal force.Estimates.Rotating bodies.Pamadi Bandu N.1945-727368Taylor Lawrence W.Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Division,OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOOCLCQGPOBOOK9910707805703321Semiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane3439928UNINA