Call Number (LC) Title Results
NAS 1.12:144 The evolution of massive stars. 1
NAS 1.12:145 An investigation of the vibration characteristics of pressurized thin-walled circular cylinders partly filled with liquid / 1
NAS 1.12:146 Laminar boundary-layer separation induced by flares on cylinders at zero angle of attack / 1
NAS 1.12:147 Computation of satellite orbits by the Hansen method as modified by Musen / 1
NAS 1.12:148 The critical inclination problem in satellite orbit theory / 1
NAS 1.12:149 Aerodynamic analysis of tektites and their parent bodies / 1
NAS 1.12:150 Theoretical study of camber flutter characteristics of monocoque and multiweb wings / 1
NAS 1.12:151 A study of guidance to reference trajectories for lifting reentry at supercircular velocity / 1
NAS 1.12:152 The aerodynamic design of wings with cambered span having minimum induced drag / 1
NAS 1.12:153 An experimental study of the pressure and heat-transfer distribution on a 70° sweep slab delta wing in hypersonic flow / 1
NAS 1.12:154 Radiant heat transfer to absorbing gases enclosed between parallel flat plates with flow and conduction / 1
NAS 1.12:155 Spin dynamics of manned space stations / 1
NAS 1.12:156 Radiant heat transfer to absorbing gases enclosed in a circular pipe with conduction, gas flow, and internal heat generation / 1
NAS 1.12:157 Radiative heat transfer between planar surfaces with filleted junctures / 1
NAS 1.12:158 Tables for eccentric and true anomaly in elliptic orbits / 1
NAS 1.12:159 Solutions of the ionized radiating shock layer : including reabsorption and foreign species effects, and stagnation region heat transfer / 1
NAS 1.12:160 Considerations of the motion of a small body in the vicinity of the stable libration points of the earth-moon system / 1
NAS 1.12:161 Theoretical and experimental study of the interaction of free-surface waves on liquid metals with transverse magnetic fields (one-dimensional unsteady waves) / 1
NAS 1.12:162 A theory of space-probe entry under conditions of high mass loss / 1
NAS 1.12:163 Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet / 1