Result Number | Material Type | Add to My Shelf Action | Record Details and Options |
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1 |
Material Type: Reports
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Air-Flow Behavior Over the Wing of an XP-51 Airplane as Indicated by Wing-Surface Tufts at Subcritical and Supercritical SpeedsPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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2 |
Material Type: Reports
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3 |
Material Type: Reports
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An experimental and theoretical study of the effect of fuel on pitching-translation flutterPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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4 |
Material Type: Reports
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Flight and analytical methods for determining the coupled vibration response of tandem helicoptersPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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5 |
Material Type: Reports
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Flight measurements of the vibrations encountered by a tandem helicopter and a method for measuring the coupled response in flightPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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6 |
Material Type: Reports
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Visualization of rotor tip secondary flows with blade tip air discharge and suction in a low-speed turbinePublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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7 |
Material Type: Reports
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An analog study of the relative importance of various factors affecting roll couplingPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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8 |
Material Type: Reports
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Simulator studies of a simple homing systemPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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9 |
Material Type: Reports
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Visualization study of secondary flows in turbine rotor tip regionsPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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10 |
Material Type: Reports
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PHASE EQUILIBRIUM RELATIONSHIPS IN THE SYSTEM K2O-FEO-AL2O3-SIO2APPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
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11 |
Material Type: Reports
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A study of the effects of body shape on the vortex wakes of inclined bodies at a Mach number of 2Public Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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12 |
Material Type: Reports
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Heat Capacity Lag in GasesPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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13 |
Material Type: Reports
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Preliminary investigation of molybdenum disulfide-air-mist lubrication for roller bearings operating to DN values of 1 x 10(exp 6) and ball bearings operating to temperatures of 1000 degrees FPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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14 |
Material Type: Reports
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An Electrical Technique for Ground Water Velocity MeasurementOCLC: #Digital Resources/Online E-Resources |
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15 |
Material Type: Reports
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16 |
Material Type: Reports
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CHROMIUM-OXYGEN AND CHROMIUM-NITROGEN EQUILIBRIUM SYSTEMSAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
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17 |
Material Type: Reports
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Smoke study of nozzle secondary flows in a low-speed turbinePublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |
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18 |
Material Type: Reports
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CHROMIUM-OXYGEN AND CHROMIUM-NITROGEN EQUILIBRIUM SYSTEMSAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
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19 |
Material Type: Reports
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CHROMIUM-OXYGEN AND CHROMIUM-NITROGEN EQUILIBRIUM SYSTEMSAPPROVED FOR PUBLIC RELEASEDigital Resources/Online E-Resources |
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20 |
Material Type: Reports
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An investigation of the use of rocket-powered models for gust-load studies with an application to a tailless swept-wing model at transonic speedsPublic Public Domain No Copyright, Unclassified, Unlimited, Publicly availableDigital Resources/Online E-Resources |