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.)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
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)
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]
Description of the design characteristics of a new all-metal, single-seat trainer glider including description of wings, fuselage, tail unit and controls
Evaluation of in-flight simulation using a helicopter of variable stability and control with regard to its use as an auxiliary in aircraft development(Evaluation of in-flight simulation of flying platform using helicopter with variable stability and maneuverability)
Flight measurements of some of the flying qualities and stability derivatives of a supersonic fighter airplane(Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter aircraft)