Call Number (LC) Title Results
NAS 1.15:X-525 A simplified method for estimating subsonic lift-curve slope at low angles of attack for irregular planform wings / 1
NAS 1.15:X-601-69-373 Summary of particle populations in the magnetosphere / 1
NAS 1.15:X-641-69-441 Turbulence from the distribution function point of view / 1
NAS 1.15:X-641-71-420 Apollo galactic x-ray astronomy observations : preliminary science report / 1
NAS 1.15:X-643-66-133 Computation of general planetary perturbations for resonance cases / 1
NAS 1.15:X-651-71-417 Aircraft measurements of microwave emission from Arctic sea ice / 1
NAS 1.15:X-690-75-42 The complex magnetic field of Jupiter / 1
NAS 1.15:X-692-70-268 Magnetic and kinetic pressures in the solar wind / 1
NAS 1.15:X-948 Photographic study of liquid-oxygen boiling and gas injection in the injector of a chugging rocket engine / 1
NAS 1.15:X-1094 Postflight evaluation of Atlas-Centaur AC-3 (launched June 30, 1964) / 1
NAS 1.15:X-1170 Interface tests for evaluating ability of pressure-suited subjects to perform lunar scientific tasks / 1
NAS 1.15:X-1464 Automated data collection system applied to Hall effect and resistivity measurements / 1
NAS 1.15:X-1572 Comparative study of mixed- and isolated-flow methods for cooled-turbine performance analyses / 1
NAS 1.15:X-1654 Lighting in cryogenic and noncryogenic fluids / 1
NAS 1.15:X-1701 Hypersonic aerodynamic characteristics of a model of low-fineness-ratio variable-geometry logistics spacecraft concept / 1
NAS 1.15:X-1702 Minimization of optical scattering effects through the use of optimal monochromator slit geometry / 1
NAS 1.15:X-1734 Thermal and dielectric properties of a homogeneous moon based on microwave and infrared temperature observations / 1
NAS 1.15:X-1740 FORTRAN programs for calculating wind-tunnel boundary interference / 1
NAS 1.15:X-1816 Transonic aerodynamic characteristics of two hypersonic cruise configurations / 1
NAS 1.15:X-1840 Effect of hypersonic research engine installation on aerodynamic characteristics of 0.0667-scale model of X-15A-2 airplane at Mach numbers from 1.75 to 4.63 / 1