Call Number (LC) Title Results
NAS 1.15:3003 STAR adaptations for two algorithms used on serial computers / 1
NAS 1.15:3004 Optical measurement of static temperature and hydroxyl radical profiles in a hydrogen-fueled supersonic combustor / 1
NAS 1.15:3005 Experimental transient turbine vane temperatures in a cascade for gas stream temperature cycling between 922 and 1644 K (1200̊ and 2500̊ F) / 1
NAS 1.15:3006 Cold-air annular-cascade investigation of aerodynamic performance of cooled turbine vanes / 1
NAS 1.15:3007 Jet engine exhaust emissions of high-altitude commercial aircraft projected to 1990 / 1
NAS 1.15:3008 Flight investigation of the VFR and IFR landing approach characteristics and terminal area airspace requirements for a light STOL airplane / 1
NAS 1.15:3009 Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects / 1
NAS 1.15:3010 Summary of recent short-haul systems studies / 1
NAS 1.15:3011 Wind tunnel blockage and support interference effects on winged-body models at Mach numbers from 0.6 to 1.0 / 1
NAS 1.15:3012 Frequency response of an axial-flow compressor exposed to inlet pressure perturbations / 1
NAS 1.15:3013 Some propulsion system noise data handling conventions and computer programs used at the Lewis Research Center / 1
NAS 1.15:3014 HYDES : a generalized hybrid computer program for studying turbojet or turbofan engine dynamics / 1
NAS 1.15:3015 Drag and distribution measurements of single-element fuel injectors for supersonic combustors / 1
NAS 1.15:3016 Wind-tunnel investigation of simulated helicopter engine exhaust interacting with windstream / 1
NAS 1.15:3017 Effect of screen-induced total-pressure distortion on axial-flow compressor stability / 1
NAS 1.15:3018 Random-access technique for modular bathymetry data storage in a contnental shelf wave refraction program. 1
NAS 1.15:3019 Effects of Reynolds number and model support on the supersonic aerodynamic characteristics of a 140̊-included-angle cone / 1
NAS 1.15:3020 Computer program for solving gains required for steady-state decoupling of elements of longitudinal mode of an airplane / 1
NAS 1.15:3021 Thermionic performance of a cesium diminiode with relatively impure 110-tungsten electrodes / 1
NAS 1.15:3022 Comparison of cooling effectiveness of turbine vanes with and without film cooling / 1