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NAS 1.14:D-6893
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Effect of high-temperature creep and oxidation on residual room-temperature properties for several thin-sheet superalloys / |
1 |
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NAS 1.14:D-6894
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Drag characteristics of a disk-gap-band parachute with a nominal diameter of 1.65 meters at Mach numbers from 2.0 to 3.0 / |
1 |
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NAS 1.14:D-6895
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Numerical analysis of the transient response of an axisymmetric ablative char layer considering internal flow effects / |
1 |
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NAS 1.14:D-6896
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The Effects of configuration changes on the aerodynamic characteristics of a full-scale mockup of a light twin-engine airplane / |
1 |
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NAS 1.14:D-6897
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Effect of jet convergence angle on the performance of annular nozzles with semitoroidal concave plugs at Mach numbers up to 1.82 / |
1 |
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NAS 1.14:D-6898
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Fixed-base simulator study of an externally blown flap STOL transport airplane during approach and landing / |
1 |
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NAS 1.14:D-6899
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Fatigue crack growth from a circular hole with and without high prior loading / |
1 |
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NAS 1.14:D-6900
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Effect of stabilization on vtol aircraft on hovering flight / |
1 |
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NAS 1.14:D-6901
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Atmospheric electricity criteria guidelines for use in aerospace vehicle development / |
1 |
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NAS 1.14:D-6902
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The interaction of moderately strong shock waves with thick perforated walls of low porosity / |
1 |
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NAS 1.14:D-6903
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An etiological study of phthalate self-contamination of spacecraft and contamination from their earthly environs / |
1 |
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NAS 1.14:D-6904
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A flight evaluation of methods for predicting vortex wake effects on trailing aircraft / |
1 |
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NAS 1.14:D-6905
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Lateral stability and control derivatives of a jet fighter airplane extracted from flight test data by utilizing maximum likelihood estimation / |
1 |
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NAS 1.14:D-6906
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Simulation study of the lift-roll problem for hovering VTOL aircraft / |
1 |
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NAS 1.14:D-6907
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Turbulent boundary-layer velocity profiles on a nonadiabatic flatplate at Mach number 6.5 / |
1 |
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NAS 1.14:D-6908
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Effects of wall cooling and angle of attack on boundary-layer transition on sharp cones at M[mathematical symbol for infinity] = 7.4 / |
1 |
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NAS 1.14:D-6909
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Dynamic stability derivatives at angles of attack from -5̊ to 90̊ for a variable-sweep fighter configuration with twin vertical tails / |
1 |
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NAS 1.14:D-6910
|
Flight test of an erectable spacecraft used for decelerator testing at simulated Mars entry conditions / |
1 |
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NAS 1.14:D-6911
|
Structure of zirconium-93 and zirconium-91 as shown by the reactions ⁹²Zr(d,p)⁹³Zr and ⁹²Zr(d,t)⁹¹Zr / |
1 |
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NAS 1.14:D-6912
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Influence of alloying elements on friction and wear of copper / |
1 |
