Result Number | Material Type | Add to My Shelf Action | Record Details and Options |
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11 |
Material Type: Report
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FACTORS IN EVALUATING FATIGUE LIFE ON STRUCTURAL PARTSIllg, W.Legacy CDMS 1960Sem texto completo |
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12 |
Material Type: Report
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13 |
Material Type: Report
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SOLUTIONS FOR COMPLEX SYSTEMS OF CHEMICAL REACTION KINETICS. PART I. SUPPLEMENT I. AN IRREVERSIBLE UNIMOLECULAR REACTION FOLLOWED BY A SECOND IRREVERSIBLE UNIMOLECULAR REACTIONKONOWALOW,DANIEL D ; BLAIR,JAMES E1960Texto completo disponível |
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14 |
Material Type: Report
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Ducts of combustible materials for heating systemsHutcheon, N. B.National Research Council of Canada 1960Sem texto completo |
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15 |
Material Type: Report
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CORPUSCULAR RADIATION EXPERIMENT OF SATELLITE 1959 IOTS /EXPLORER VIILudwig, G. H. ; Whelpley, W. A.Legacy CDMS 1960Sem texto completo |
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16 |
Material Type: Report
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Precise Measurement of Heat of Combustion with a Bomb CalorimeterJessup, R. S ; United States. Bureau of StandardsUnited States. Government Printing Office 1960Sem texto completo |
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17 |
Material Type: Report
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Temperature reducing coating for metals subject to flame exposure PatentKatz, N. H. ; Simon, S. L.Legacy CDMS 1960Texto completo disponível |
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18 |
Material Type: Report
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MEASUREMENT OF STRUCTURAL INFLUENCE COEFFICIENTSLauten, W. T., Jr ; Martin, D. J.Legacy CDMS 1960Sem texto completo |
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19 |
Material Type: Report
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Heat-transfer Measurements on a Blunt Spherical-segment Nose to a Mach Number of 15.1 and Flight Performance of the Rocket-propelled Model to a Mach Number of 17.8Lee, D. B. ; Rumsey, C. B.Legacy CDMS 1959Texto completo disponível |
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20 |
Material Type: Report
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Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0Chiccine, B. G. ; Shinn, A. M., Jr ; Valerino, A. S.Legacy CDMS 1959Texto completo disponível |