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Hispano Aviacien S A
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Hispano Aviacien S A
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Application filed by Hispano Aviacien S AfiledCriticalHispano Aviacien S A
Priority to ES0234096ApriorityCriticalpatent/ES234096A1/es
Publication of ES234096A1publicationCriticalpatent/ES234096A1/es
Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets
(AREA)
Abstract
Procedimiento para modificar la estabilidad de un avión, consistente en variar la posición de su dentro de gravedad de una manera ficticia, de acuerdo con la posición que puede tomar el punto neutro, valiéndose de una superficie sustentadora situada a una cierta distancia del centro de gravedad del avión que de lugar a una fuerza aerodinámica equivalente en magnitud y con igual dirección o dirección contraria, a la que daría lugar sobre el avión, debido a las aceleraciones a que está sometido en vuelo una masa ligada a un punto de éste.
ES0234096A1957-03-071957-03-07Procedimiento para modificar la estabilidad de un aviën
ExpiredES234096A1
(es)
Effects of components and various modifications on the drag and the static stability and control characteristics of a 42 deg swept-wing fighter-airplane model at Mach numbers of 1. 60 to 2. 50(Wind tunnel testing of swept wing fighter aircraft model for determining drag and static longitudinal and lateral stability and control characteristics)
V/stol handling qualities as determined by flight test and simulation techniques(Bell X-14 A test vehicle used to determine control power and damping requirements for V/STOL AIRCRAFT)