Search U.S. government technical reports digitized or harvested by TRAIL.
Estimation of incremental pitching moments due to trailing-edge flaps on swept and triangular wings
An experimental and theoretical study of the effect of fuel on pitching-translation flutter
Experimental investigation of lift, drag, and pitching moment of five annular airfoils
Experimental investigation of cermet turbine blades in an axial-flow turbojet engine
Experimental investigation of deposition by boron-containing fuels in turbojet combustor
Experimental investigation of ejector-nozzle metal temperatures
Some experimental studies of panel flutter at Mach number 1.3
Some Reynolds number phenomena in a turbojet compressor
Some research results on sandwich structures
Studies of structural failure due to acoustic loading
The response of an airplane to random atmospheric disturbances
Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range
Static-pressure error calibrations for nose-boom airspeed installations of 17 airplanes
A study of sprays formed by two impinging jets
Survey of the acoustic near field of three nozzles at a pressure ratio of 30
Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds
Screen-type noise reduction devices for ground running of turbojet engines
In-flight gains realized by modifying a twin side-inlet induction system
Induced velocities near a lifting rotor with nonuniform disk loading
A theory for the lateral response of airplanes to random atmospheric turbulence
Theoretical and experimental investigations of delta-wing vibrations