Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Vickers Armstrongs Aircraft Ltd
Original Assignee
Vickers Armstrongs Aircraft Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Vickers Armstrongs Aircraft LtdfiledCriticalVickers Armstrongs Aircraft Ltd
Priority to GB3955559ApriorityCriticalpatent/GB910792A/en
Priority to ES0262582Aprioritypatent/ES262582A1/es
Priority to NL258193Aprioritypatent/NL110890C/xx
Publication of GB910792ApublicationCriticalpatent/GB910792A/en
Rational calculation of design gust loads in relation to present and proposed airworthiness requirements(Effect of gust loads on wing and T-tail airworthiness requirements for short haul aircraft)
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)
Dual-fuselage aircraft having yawable wing and horizontal stabilizer(Design of dual fuselage aircraft with pivoting wing and horizontal stabilizer to permit yawing of wing in flight for high speed operation)[Patent]