Call Number (LC) Title Results
NAS 1.12:92 An investigation of the effect of high temperature on the Schumann-Runge ultraviolet absorption continuum of oxygen / 1
NAS 1.12:93 Theoretical and experimental investigation of supercavitating hydrofoils operating near the free water surface / 1
NAS 1.12:94 Similarity of near noise fields of subsonic jets / 1
NAS 1.12:95 Shielding of partially reflecting stagnation surfaces against radiation by transpiration of an absorbing gas / 1
NAS 1.12:96 Analysis of multipoint-multitime correlations and diffusion in decaying homogeneous turbulence / 1
NAS 1.12:97 Considerations affecting satellite and space probe research with emphasis on the "scout" as a launch vehicle / 1
NAS 1.12:98 Hot-wire calorimetry : theory and application to ion rocket research / 1
NAS 1.12:99 Theory of the secular variations in the orbit of a satellite of an oblate planet / 1
NAS 1.12:100 Collection of zero-lift drag data on bodies of revolution from free-flight investigations / 1
NAS 1.12:101 Theoretical prediction of the effects of vortex flows on the loading, forces, and moments of slender aircraft / 1
NAS 1.12:102 An Analysis of errors and requirements of an optical guidance technique for approaches to atmospheric entry with interplanetary vehicles / 1
NAS 1.12:103 Theoretical elastic stress distributions arising from discontinuities and edge loads in several shell-type structures / 1
NAS 1.12:104 Local heat transfer and recovery temperatures on a yawed cylinder at a mach number of 4.15 and high Reynolds numbers / 1
NAS 1.12:105 Sputtering of metals by mass-analyzed N+, and N+ / 1
NAS 1.12:106 Tables of z functions for atmosphere entry analyses / 1
NAS 1.12:107 Similarity solutions for small cross flows in laminar compressible boundary layers / 1
NAS 1.12:108 Measurements of the dissociation rate of molecular oxygen / 1
NAS 1.12:109 Hypersonic viscous shock layer of nonequilibrium dissociating gas [with list of references] / 1
NAS 1.12:110 Analytical method of approximating the motion of a spinning vehicle with variable mass and inertia properties acted upon by several disturbing parameters / 1
NAS 1.12:111 Theoretical performance of hydrogen-oxygen rocket thrust chambers / 1