1-12 of 12 Books
The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel
The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel
By Norbert Ulbrich
Assessment of dual-point drag reduction for an executive-jet modified airfoil section
Assessment of dual-point drag reduction for an executive-jet modified airfoil section
By Dennis O. Allison
Validation of vortex-lattice method for loads on wings in lift-generated wakes
Validation of vortex-lattice method for loads on wings in lift-generated wakes
By Vernon J. Rossow
Turbine blade-tip clearance excitation forces
Turbine blade-tip clearance excitation forces
By Manuel Martinez-Sanchez
Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
By Marc W. Kniskern
Manipulation of micro scale particles in an optical trap using interferometry
Manipulation of micro scale particles in an optical trap using interferometry
By Robin Seibel
Force balance and substorm effects in the magnetotail
Force balance and substorm effects in the magnetotail
By Richard L. Kaufmann
Expanded equations for torque and force on a cylindrical permanent magnet core in a large-gap magnetic suspension system
Expanded equations for torque and force on a cylindrical permanent magnet core in a large-gap magnetic suspension system
By Nelson J. Groom
Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler
Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler
By W. H. Wentz
Bubble generation in a continuous liquid flow under gravity conditions
Bubble generation in a continuous liquid flow under gravity conditions
By Salvatore Cezar Pais
A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas
A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas
By Robert J. Mack
Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction
Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction
By Stephen E. Dunagan