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.)
RECH S POUR L APPLIC IND DES B
Original Assignee
RECH S POUR L APPLIC IND DES B
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 RECH S POUR L APPLIC IND DES BfiledCriticalRECH S POUR L APPLIC IND DES B
Application grantedgrantedCritical
Publication of FR1113078ApublicationCriticalpatent/FR1113078A/en
B64C9/00—Adjustable control surfaces or members, e.g. rudders
Landscapes
Engineering & Computer Science
(AREA)
Aviation & Aerospace Engineering
(AREA)
FR1113078D1954-05-151954-05-15
Device for controlling the forces exerted in flight on the airfoil of an airplane and other flying machines
ExpiredFR1113078A
(en)
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)
A possibility for avoiding surface roughness caused by insects on aircraft(Use of elastic surfaces on wing leading edges and fuselage edges of aircraft with boundary layer control, to avoid surface roughness due to insects)