GB820009A - Improvements in or relating to aircraft capable of flight at supersonic speeds - Google Patents

Improvements in or relating to aircraft capable of flight at supersonic speeds

Info

Publication number
GB820009A
GB820009A GB10219/56A GB1021956A GB820009A GB 820009 A GB820009 A GB 820009A GB 10219/56 A GB10219/56 A GB 10219/56A GB 1021956 A GB1021956 A GB 1021956A GB 820009 A GB820009 A GB 820009A
Authority
GB
United Kingdom
Prior art keywords
aircraft
mach
supersonic speeds
flight
relating
Prior art date
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.)
Expired
Application number
GB10219/56A
Inventor
Werner Joseph Georg Pinsker
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.)
Minister of Supply In Her Majesty S Government
Original Assignee
Minister of Supply In Her Majesty S Government
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 Minister of Supply In Her Majesty S Government filed Critical Minister of Supply In Her Majesty S Government
Priority to GB10219/56A priority Critical patent/GB820009A/en
Publication of GB820009A publication Critical patent/GB820009A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/42—Adjusting about chordwise axes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Stereoscopic And Panoramic Photography (AREA)

Abstract

820,009. Controlling aircraft. MINISTER OF SUPPLY. March 22, 1957 [April 3, 1956], No. 10219/56. Drawings to Specification. Class 4. In an aircraft capable of supersonic speeds, aerodynamic surfaces are provided which are movable about an axis, parallel to the craft longitudinal axis, into either horizontal or vertical positions. The surfaces may be at the wing tips or at the tail assembly and control is effected, automatically, through a computor, in accordance with Mach number, air pressure and temperature. At speeds below Mach 0À8 the surfaces provide large pitch and small yaw contributions to the aircraft stability and above Mach 0À8 the contributions are reversed.
GB10219/56A 1956-04-03 1956-04-03 Improvements in or relating to aircraft capable of flight at supersonic speeds Expired GB820009A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB10219/56A GB820009A (en) 1956-04-03 1956-04-03 Improvements in or relating to aircraft capable of flight at supersonic speeds

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10219/56A GB820009A (en) 1956-04-03 1956-04-03 Improvements in or relating to aircraft capable of flight at supersonic speeds

Publications (1)

Publication Number Publication Date
GB820009A true GB820009A (en) 1959-09-16

Family

ID=9963798

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10219/56A Expired GB820009A (en) 1956-04-03 1956-04-03 Improvements in or relating to aircraft capable of flight at supersonic speeds

Country Status (1)

Country Link
GB (1) GB820009A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2130159A (en) * 1982-11-18 1984-05-31 Messerschmitt Boelkow Blohm Aircraft wings provided with additional surfaces arranged at the wing tips
GB2230748A (en) * 1986-03-03 1990-10-31 Diehl Gmbh & Co Guidance mechanism for projectiles
EP0416268A2 (en) * 1989-09-04 1991-03-13 British Aerospace Public Limited Company Tail unit
FR2962971A1 (en) * 2010-07-20 2012-01-27 Airbus Operations Sas DEVICE AND METHOD FOR LATERAL STABILIZATION OF AN AIRCRAFT
JP2012081956A (en) * 2010-10-11 2012-04-26 Eads Deutschland Gmbh Variable shape aircraft
CN108910018A (en) * 2018-06-23 2018-11-30 肇庆市德诺电子科技有限公司 A kind of foldable vertical tail system of composite wing vertically taking off and landing flyer

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2130159A (en) * 1982-11-18 1984-05-31 Messerschmitt Boelkow Blohm Aircraft wings provided with additional surfaces arranged at the wing tips
GB2230748A (en) * 1986-03-03 1990-10-31 Diehl Gmbh & Co Guidance mechanism for projectiles
GB2230748B (en) * 1986-03-03 1991-03-20 Diehl Gmbh & Co Projectile guidance apparatus.
EP0416268A2 (en) * 1989-09-04 1991-03-13 British Aerospace Public Limited Company Tail unit
EP0416268A3 (en) * 1989-09-04 1991-04-03 British Aerospace Public Limited Company Tail unit
US5096143A (en) * 1989-09-04 1992-03-17 William Nash Tail unit with rotatable tailplane
FR2962971A1 (en) * 2010-07-20 2012-01-27 Airbus Operations Sas DEVICE AND METHOD FOR LATERAL STABILIZATION OF AN AIRCRAFT
WO2012017152A1 (en) * 2010-07-20 2012-02-09 Airbus Operations (Sas) Method and device for the lateral stabilization of an aircraft
US8888039B2 (en) 2010-07-20 2014-11-18 Airbus Operations Sas Method and device for the lateral stabilization of an aircraft
JP2012081956A (en) * 2010-10-11 2012-04-26 Eads Deutschland Gmbh Variable shape aircraft
EP2439138A3 (en) * 2010-10-11 2017-07-12 Airbus Defence and Space GmbH Flying device with variable geometry
CN108910018A (en) * 2018-06-23 2018-11-30 肇庆市德诺电子科技有限公司 A kind of foldable vertical tail system of composite wing vertically taking off and landing flyer

Similar Documents

Publication Publication Date Title
GB884128A (en) Improvements in or relating to flying bodies for supersonic speeds
GB820009A (en) Improvements in or relating to aircraft capable of flight at supersonic speeds
GB1157822A (en) VTOL Aircraft
GB861480A (en) Improvements in aircraft
GB697721A (en) Improvements in or relating to flying bodies
GB786778A (en) Improvements in or relating to machines for sonic or supersonic flight
GB987792A (en) Improvements in and relating to aircraft wings
GB834532A (en) Improvements in or relating to wings and other main support aerofoils in aircraft
GB871713A (en) Improvements in or relating to aerodynes
GB796400A (en) Improvements relating to air intakes for aircraft power plant installations
GB567072A (en) Screw and jet propelled aircraft
GB679445A (en) Improvements in aircraft
GB576120A (en) Improvements relating to the control of aircraft
GB862476A (en) Improvements in jet-propelled aircraft
GB1022952A (en) Jet propulsion gas turbine engines
GB881663A (en) Improvements in or relating to gas turbine propulsion units
ALFORD Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration(Wind tunnel studies at supersonic and transonic speeds to determine aerodynamic characteristics of variable sweep wing aircraft- configuration)
Carmel et al. Investigation of drag and static longitudinal and lateral stability characteristics of a model of a 40. 4 deg swept-wing airplane at Mach numbers of 1. 56 and 2. 06(Wind tunnel test to determine swept wing fighter aircraft drag, and logitudinal and lateral stablity at supersonic speeds)
Daugherty et al. Wind Tunnel Investigation at Supersonic Speeds of the Lift, Drag, Static- Stability and Control Characteristics of a 0. 03-Scale Model of an Interim Development Version of the B-70 Airplane
APPICH Aerodynamic characteristics of three versions of a supersonic airplane model with a 45 deg sweptback midwing at Mach numbers of 1. 57 and 2. 01(Stability and drag studies for configurations of supersonic swept wing jet aircraft model at Mach numbers 1. 57 and 2. 01)
BRIGHT et al. Effects of deflected wing tips on the aero- dynamic characteristics of a canard configuration at mach numbers from 0. 7 to 3. 5(Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected wing tips for longitudinal and directional stability)
GB856507A (en) Improvements in supersonic airfoil
KUCHEMANN Aerodynamic development of thin wings for supersonic aircraft
GB732617A (en) Improvements in or relating to wing units and the like for aircraft
MCLEMORE et al. Low-speed wind tunnel tests of 1/9-scale model of a variable-sweep supersonic cruise aircraft(conducted in the Langley full-scale wind tunnel)