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Vickers Armstrongs Aircraft Ltd
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Vickers Armstrongs Aircraft Ltd
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Publication date
Application filed by Vickers Armstrongs Aircraft LtdfiledCriticalVickers Armstrongs Aircraft Ltd
Priority to ES0251904ApriorityCriticalpatent/ES251904A2/es
Publication of ES251904A2publicationCriticalpatent/ES251904A2/es
Mejoras introducidas en el objeto de la patente principal núm. 251.737, por "un aerodino para vuelo a velocidades supersónicas y subsónicas bajas", consistentes en que la forma de planta del ala delantera es un triángulo finamente puntiagudo cuyos bordes de ataque quedan dentro de las líneas rectas que unen la proa con los extremos de la base, merced a lo cual se obtiene la deseada relación reducida de espesor a cuerda, sin aumento de la resistencia de arrastre.
ES0251904A1959-09-041959-09-04Un aerodino para vuelo a veloidades supersënicas y subsënicas bajas
ExpiredES251904A2
(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)
Equations for the longitudinal control of an aircraft in which the elevator aerodynamic balance varies with the speed at which the aircraft is longitudinally balanced
Longitudinal and Lateral Stability and Control Characteristics of a 1/9-Scale Model of a Twin-Ramjet Canard Target Drone at Mach Numbers from 0. 60 to 2. 80