NAS 1.14:D-7828
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Analysis of validation tests of the Langley pilot transonic cryogenic tunnel / |
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NAS 1.14:D-7829
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Four-dimensional guidance algorithms for aircraft in an air traffic control environment / |
1 |
NAS 1.14:D-7830
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Effects of time-shifted data on flight-determined stability and control derivatives / |
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NAS 1.14:D-7832
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25-mb sounding data and synoptic charts for NASA's AVE II Pilot Experiment / |
1 |
NAS 1.14:D-7833
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Comparison of three methods for calculation of helicopter rotor blade loading and stresses due to stall / |
1 |
NAS 1.14:D-7834
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Application of a parameter identification technique to a hingeless helicopter rotor / |
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NAS 1.14:D-7835
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Weak incident shock interactions with Mach 8 laminar boundary layers / |
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NAS 1.14:D-7836
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Aerodynamic performance of 0.5-meter-diameter, 337-meter-per-second tip speed, 1.5-pressure-ratio, single-stage fan designed for low noise aircraft engines / |
1 |
NAS 1.14:D-7837
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Operating characteristics of 120-millimeter-bore ball bearings at 3x10⁶ DN / |
1 |
NAS 1.14:D-7838
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Effects of alloy composition in alleviating embrittlement problems associated with the tantalum alloy T-111 / |
1 |
NAS 1.14:D-7839
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Analysis of the dynamic response of a supersonic inlet to flow-field perturbations upstream of the normal shock / |
1 |
NAS 1.14:D-7840
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Surface recrystallization theory of the wear of copper in liquid methane / |
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NAS 1.14:D-7842
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Minimization of sonic-boom parameters in real and isothermal atmospheres. |
1 |
NAS 1.14:D-7843
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Description and flight test results of the NASA F-8 digital fly-by-wire control system : a collection of papers from the NASA Symposium on Advanced Control Technology, Los Angeles, Calif., July 9-11, 1974. |
1 |
NAS 1.14:D-7844
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Mechanical properties of Skylab thermal shield materials after prolonged ultraviolet irradiation / |
1 |
NAS 1.14:D-7845
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A computer program for calculation of spectral radiative properties of gas mixtures / |
1 |
NAS 1.14:D-7846
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Reliability approach to rotating-component design / |
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NAS 1.14:D-7847
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Hardness behavior of binary and ternary niobium alloys at 77 and 300 K / |
1 |
NAS 1.14:D-7848
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Experimental and analytical sonic nozzle discharge coefficients for Reynolds numbers up to 8x10⁶ / |
1 |
NAS 1.14:D-7849
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Decomposition of nitric oxide in a hot nitrogen stream to synthesize air for hypersonic-wind-tunnel combustion testing / |
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