000 00963 a2200109 4500
100 _aComputational Fluid Dynamics Branch
245 _aNasa technical report [TR R-386]
_bConvection in the tanks of a rotating spacecraft
_cNASA
260 _aNational aeronautics and space adminstration washington, D.C
_bNASA
_c1972
300 _a137p
500 _a TR002275 : [ TR R-387] Maximum range three- dimensional lifting planetary entry by Dickmanns, E. D TR002276 : [TR R-388] An implicit finite-difference solution to the viscous shock layer including the effects of radiation and strong blowing by Garrett, Bernard L. TR002277 : [TR R-389] Experimental determination of potential lunar surface organic contamination in the lunar module descent-engine exhaust by Flory, Donald A. TR002278 : [TR R-391] Measurement of the structure and circulation of the stratosphere and mesosphere,1970
942 _cTR
999 _c566872
_d566872