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 |