000 | 02352nam a22003257a 4500 | ||
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003 | OSt | ||
040 | _cIIT Kanpur | ||
041 | _aeng | ||
110 | _aWashington. National Aeronautics and Space Administration (NASA) | ||
245 | _aNASA Technical Note [D- 3444-59] | ||
260 |
_aWashington _bNASA _c1966 |
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440 | _aNational Aeronautics and Space Administration | ||
440 | _aNASA Technical Note | ||
500 | _aLack nos. 3446, 3447, 3450, 3455 | ||
500 | _aNASA TN D-3444 -- An experimental study of the oxidation of graphite in high-temperature supersonic and hypersonic environments/ Irvin M. Miller and Kenneth Sutton | ||
500 | _aNASA TN D-3445 -- Evaluation of special 301-type stainless steel for improved low-temperature notch toughness of cryoformed pressure vessels/ Thomas W. Orange | ||
500 | _aNASA TN D-3448 -- Energy transport by thermal field emission/ James F. Morris | ||
500 | _aNASA TN D-3449 -- Effects of subcooling and gravity level on boiling in the discrete bubble region/ Thomas H. Cochran and John C. Aydelott | ||
500 | _aNASA TN D-3451 -- Prediction of propellant tank pressurization requirements by dimensional analysis/ J. F. Thompson and M. E. Nein | ||
500 | _aNASA TN D-3452 -- Sets of similarity ratios for thermal modeling/ J. R. Watkins | ||
500 | _aNASA TN D-3453 -- Mathematical model with experimental verification for the dynamic behavior of a single-tube condenser/ Andrew A. Schoenberg | ||
500 | _aNASA TN D-3454 -- Effect of face-sheet stiffness on buckling of cylindrical shells of sandwich construction/ Robert E. Fulton and Nancy P. Sykes | ||
500 | _aNASA TN D-3456 -- Projectile-impact-induced fracture of liquid-filled, filament-reinforced plastic of aluminum tanks/ Francis S. Stepka | ||
500 | _aNASA TN D-3457 -- Steady-state composition of a low-density nonequilibrium hydrogen plasma/ Roman Krawec | ||
500 | _aNASA TN D-3458 -- Experimental evaluation of pressurant gas injectors during the pressurized discharge of liquid hydrogen/ Richard L. DeWitt, Robert J. Stochl and William R. Johnson | ||
500 | _aNASA TN D-3459 -- Effect of thickness and sweep angle on the longitudinal aerodynamic characteristics of slab delta planforms at a mach number of 20/ Robert D. Witcofski and Don C. Marcum | ||
650 | _aAeronautics | ||
650 | _aSpacecraft | ||
942 | _cBK | ||
999 |
_c565915 _d565915 |