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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Application of concentrated loads to fixed edge and discontinuous two-way slabs of reinforced concrete using finite difference approximation to biharmonic equation
Thunderstorm cold air outflow leading edge structure recorded by NASA meteorological tower at Kennedy Space Center
Supersonic leading edge problem solved by ellipsoidal model using discrete ordinate method compared with BGK model solution
Optimal directed circuit and cycle elimination in weighted diagraphs by edge reversal orientation
Slender wings leading edge vortex flow effect on roll damping at subsonic speeds
Electron densities between inner edge plasma sheet and plasmasphere as function of geocentric radial distance from OGO-3 electrostatic measurements
Theoretical and experimental vibration and buckling results for blunt truncated conical shells with ring supported edges
Performance of auxiliary inlet ejector nozzle with floating inlet doors and floating single hinge trailing edge flaps
Effect of static stress and edge restraint on vibration of nearly cylindrical shells with circular cross section and slight meridional curvature
Analysis of supersonic and hypersonic flow of inviscid ideal gas over conical wings with sharp leading edges and attached shock waves by three dimensional method of characteristics
Construction of leading edges of surfaces for aerial vehicles performing from subsonic to above transonic speeds
Flight-measured base pressures from sharp leading edge upper vertical fin of X-15 aircraft compared with wind tunnel data for turbulent flow at Mach numbers from 1.5 to 5.0
Supersonic asymmetric flutter and divergence characteristics of truncated conical shells with ring-supported edges under three types of flow-induced instabilities
Simple integral method for calculating real gas turbulent boundary layers with variable edge entropy and flight calculations showing effect of nose bluntness at 6.09 km/sec
Wind tunnel measurements of pressure distributions on wing having NACA 4415 airfoil sections with trailing-edge flaps set at 0 deg and 40 deg
Computerized simulation of shock waves and flow fields behind supersonic edge delta wings and wing-body combinations
Design of low cost ablator leading edge for space shuttle thermal protection system
Experimental and analytical study of subsonic longitudinal and lateral aerodynamic characteristics of slender sharp edge 74 deg swept wings