LEADER 02134oam  2200577I  450 
001 9910707805703321
005 20170110161520.0
035   $a(CKB)5470000002468506
035   $a(OCoLC)755080648
035   $a(EXLCZ)995470000002468506
100   $a20110929j198712    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSemiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane /$fBandu N. Pamadi, Lawrence W. Taylor
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Division,$dDecember 1987.
215   $a1 online resource (vii, 80 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4009
300   $a"December 1987" Report documentation page.
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 18-19).
606   $aSpin (Aerodynamics)$2fast
606   $aAerodynamic coefficients$2nasat
606   $aAerodynamic forces$2nasat
606   $aCentrifugal force$2nasat
606   $aEstimates$2nasat
606   $aRotating bodies$2nasat
615  7$aSpin (Aerodynamics)
615  7$aAerodynamic coefficients.
615  7$aAerodynamic forces.
615  7$aCentrifugal force.
615  7$aEstimates.
615  7$aRotating bodies.
700   $aPamadi$b Bandu N.$f1945-$0727368
702   $aTaylor$b Lawrence W.
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Division,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707805703321
996   $aSemiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane$93439928
997   $aUNINA