Effects of leading-edge bluntness and ramp deflection angle on laminar boundary-layer separation in hypersonic flow
Leading edge bluntness and ramp deflection angle effects on laminar boundary layer separation in hypersonic flow
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Leading edge bluntness and ramp deflection angle effects on laminar boundary layer separation in hypersonic flow
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Free flight tunnel testing of swept wing aircraft model to determine roll effectiveness of differentially deflected horizontal tail
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System locates the focal point of an extremely high intensity electron beam. The electron beam is swept and scanned cyclically with deflection coils under a focusing lens, causing the beam focal point to move so the locus of its positions is a spherical surface symmetrical to the beam axis.
Constant chord, trailing edge, control deflection effects on aerodynamic loading characteristics of 60 degree delta wing-body combination at transonic speeds
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Capsule containing samples for radiation testing is guided under through a seal to an exact position within a nuclear reactor. A Linear Variable Differential Transformer /LVDT/ flexplate deflection circuit monitors the force on the capsule as it is positioned within the reactor.
Sensor automatically and accurately measures the two-dimensional deflection angles of a laser beam to provide closed-loop servomechanism control of laser beam directivity.
Wind tunnel tests of deflected slipstream cruise fan V/STOL aircraft wing
Stiffness matrices derived for triangular shell elements associated with polyhedral deflection distributions
Performance evaluation of annular plug and expansion-deflection nozzles including external flow effects at transonic Mach numbers
Laminar flow separation on flat plate induced by deflected trailing-edge flap at hypersonic speed
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Mean square deflection of charged particles by current carrying plasma
Invariants of triangular shell element stiffness matrices associated with polyhedral deflection distribution, discussing effect of geometry
Separated flow region within planar expansion- deflection nozzle investigated by supersonic smoke tunnel, discussing base pressure
Asymmetrically loaded shells of revolution nonlinear deflections analyzed by algorithm, determining snap buckling load of shallow spherical shell