PERFORMANCE CHARACTERISTICS OF SEVERAL DIVERGENT-SHROUD AIRCRAFT EJECTORS
Performance characteristics of several divergent- shroud aircraft ejectors
SEARCH · Search NASA
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Performance characteristics of several divergent- shroud aircraft ejectors
Off-design performance of divergent ejectors
Predicting flutter and divergence of unswept wings at subsonic & supersonic speeds
Radiative divergence and effect on temperature profile and dynamics of atmosphere
Numerical solutions of free molecular flow in converging and diverging tubes and slots
Flux patterns from free molecular gas flow through converging and diverging slots
Solar beam divergence effects on thermal characteristics of spacecraft tested in solar simulator
Solar beam divergence effects on thermal characteristics of spacecraft tested in solar simulator
Discrete system matrix method for analyzing aeroelastic divergence behavior of unguided slender body launch vehicles
Static aeroelastic divergence characteristics of delta-planform model of canard control surfaces
Stress in viscoelastic polystyrene in Aroclor flowing in straight, converging and diverging channels
Low thrust divergent flow cesium-on-tungsten contact ionization electrostatic thrustor for satellite attitude control and stationkeeping missions
Divergent-beam diffraction geometry for interpretation of Kossel diffraction patterns in space group assignment lattice parameters and structure factor evaluation
Dipole moment approximation of three-dimensional plasma acceleration through axisymmetric diverging magnetic fields
Two-dimensional panel flutter and panel divergence in subsonic flow - wind tunnel testing of two and three-dimensional panels
Low thrust divergent flow cesium-on-tungsten contact ionization electrostatic thrustor for satellite attitude control and stationkeeping missions
Divergent-flow contact-ionization electrostatic thrustor for satellite attitude control and stationkeeping
Aeroelastic divergence characteristics of moveable control surfaces, including drag loadings