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Hispano Aviacien S A
Original Assignee
Hispano Aviacien S A
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Application filed by Hispano Aviacien S AfiledCriticalHispano Aviacien S A
Priority to ES0234096ApriorityCriticalpatent/ES234096A1/en
Publication of ES234096A1publicationCriticalpatent/ES234096A1/en
Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets
(AREA)
Abstract
Procedure to modify the stability of an airplane, consisting of varying the position of its inside gravity in a fictitious manner, according to the position that the neutral point can take, using a bearing surface located at a certain distance from the center of gravity of the airplane that gives rise to an aerodynamic force equivalent in magnitude and with the same direction or opposite direction, to which it would give place on the airplane, due to the accelerations to which a mass linked to a point of the latter is subjected in flight. (Machine-translation by Google Translate, not legally binding)
ES0234096A1957-03-071957-03-07Procedure to modify the stability of an aircraft (Machine-translation by Google Translate, not legally binding)
ExpiredES234096A1
(en)
A compensation device for gyroscopic effects intended for aircraft and aerodines equipped with turbo-machines (Machine-translation by Google Translate, not legally binding)
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)