Call Number (LC) Title Results
NAS 1.14:D-5102 Large-scale tests of an airplane model with a double-Delta wing, including longitudinal and lateral characteristics and ground effects / 1
NAS 1.14:D-5103 Resonant mode analysis of the Fitzgerald apparatus / 1
NAS 1.14:D-5104 Investigation of occultation and imagery problems for orbital missions to Venus and Mars / 1
NAS 1.14:D-5105 Effect of gravitational-model selection on accuracy of lunar orbit determination from short data arcs / 1
NAS 1.14:D-5106 The design and uncertainty analysis of an improved total hemispherical emittance transient calorimeter / 1
NAS 1.14:D-5107 On lateral cable oscillations of cable-connected space stations / 1
NAS 1.14:D-5108 Effects of bottom-structure flexibility on water landing loads of Apollo spacecraft models / 1
NAS 1.14:D-5109 Calorimetric evaluation of two cone-column solar-energy concentrators / 1
NAS 1.14:D-5110 Tables of Mie scattering functions for particles with refractive index 1.5 /
Tables of Mie scattering cross sections and amplitudes /
2
NAS 1.14:D-5111 Simulation of package transfer concepts for Saturn I Orbital Workshop / 1
NAS 1.14:D-5112 Symbol-oriented failure analysis in multicomponent systems / 1
NAS 1.14:D-5113 Use of tungsten-184 as a thermal flux monitor at high temperatures / 1
NAS 1.14:D-5114 Low-density foam for insulating liquid-hydrogen tanks / 1
NAS 1.14:D-5115 Effect of flow rate on the dynamic contact angle for wetting liquids / 1
NAS 1.14:D-5116 Mathematical analysis of the Fitzgerald apparatus / 1
NAS 1.14:D-5117 Optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints / 1
NAS 1.14:D-5118 Response of an infinite elastic plate to axisymmetric initial velocity distributions with application to hypervelocity impact / 1
NAS 1.14:D-5119 Annealing of 22-, 40-, and 158-MeV proton damage in n- and p-type silicon / 1
NAS 1.14:D-5120 Effects of cloud cover on selection of recovery sites for future earth orbital missions / 2
NAS 1.14:D-5121 Experimental stagnation-point velocity gradients and heat-transfer coefficients for a family of blunt bodies at Mach 8 and angles of attack / 1