GB910792A - Improvements in aeroplanes having wings adjustable in sweep - Google Patents

Improvements in aeroplanes having wings adjustable in sweep

Info

Publication number
GB910792A
GB910792A GB3955559A GB3955559A GB910792A GB 910792 A GB910792 A GB 910792A GB 3955559 A GB3955559 A GB 3955559A GB 3955559 A GB3955559 A GB 3955559A GB 910792 A GB910792 A GB 910792A
Authority
GB
United Kingdom
Prior art keywords
root
sweep
wing
annulus
nov
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
GB3955559A
Other languages
English (en)
Inventor
Maurice Joseph Brennan
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 Ltd filed Critical Vickers Armstrongs Aircraft Ltd
Priority to GB3955559A priority Critical patent/GB910792A/en
Priority to ES0262582A priority patent/ES262582A1/es
Priority to NL258193A priority patent/NL110890C/xx
Publication of GB910792A publication Critical patent/GB910792A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/40Varying angle of sweep

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
  • Supports For Plants (AREA)
  • Wind Motors (AREA)
GB3955559A 1959-11-20 1959-11-20 Improvements in aeroplanes having wings adjustable in sweep Expired GB910792A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB3955559A GB910792A (en) 1959-11-20 1959-11-20 Improvements in aeroplanes having wings adjustable in sweep
ES0262582A ES262582A1 (es) 1959-11-20 1960-11-19 Mejoras introducidas en los aeroplanos
NL258193A NL110890C (enrdf_load_stackoverflow) 1959-11-20 1960-11-21

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3955559A GB910792A (en) 1959-11-20 1959-11-20 Improvements in aeroplanes having wings adjustable in sweep

Publications (1)

Publication Number Publication Date
GB910792A true GB910792A (en) 1962-11-21

Family

ID=10410182

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3955559A Expired GB910792A (en) 1959-11-20 1959-11-20 Improvements in aeroplanes having wings adjustable in sweep

Country Status (3)

Country Link
ES (1) ES262582A1 (enrdf_load_stackoverflow)
GB (1) GB910792A (enrdf_load_stackoverflow)
NL (1) NL110890C (enrdf_load_stackoverflow)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5337974A (en) * 1992-04-15 1994-08-16 The Boeing Company Wing pivot structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5337974A (en) * 1992-04-15 1994-08-16 The Boeing Company Wing pivot structure

Also Published As

Publication number Publication date
ES262582A1 (es) 1961-06-01
NL110890C (enrdf_load_stackoverflow) 1965-03-15

Similar Documents

Publication Publication Date Title
GB910792A (en) Improvements in aeroplanes having wings adjustable in sweep
GB902526A (en) Improvements in wing pivot bearings for aeroplanes having wings adjustable in sweep
GB1220055A (en) Fixed wing aeroplanes
GB679897A (en) Improvements in airplane construction
BAGLEY Summary of aerodynamic principles and various methods used in the design of swept wings for high-speed aircraft
CHOPIN et al. Transonic wind-tunnel tests on rectangular wing of aspect ratio 4
SANTINI Aeroelastic effects on helicopter rotors in unsteady conditions
YFF 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)
LACHNIT Whirling arm model for helicopter rotor tests
ROLFE Use of conventional flight instruments in helicopters, and main differences in the flight task of the helicopter as compared to the airplane
KUCHEMANN Aerodynamic development of thin wings for supersonic aircraft
LEGENDRE Determining the wing leading edge curve for supersonic aircraft, used in airfoil dimension calculations
CHURCH 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)
FIORINI Aerodynamic aspects of studies on jet-flap rotors
USD175108S (en) Airplane
BRUHA Helicopter rotor and airscrew performance based on aerodynamic characteristics
ES260949A1 (es) Mejoras en los aeroplanos
GB950400A (en) Improvements in aeroplanes
KUECHEMAN Discussion of slender wings of predominantly light-alloy construction for supersonic flight
CLARKE Helicopter dynamic loads with particular reference to high blade incidence and methods for calculating blade deformations
LETSCHER Endurance testing of rotors under simulated conditions
JONES 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]
MILLER Aerodynamic advances of hypersonic transports in performance, aeroelasticity and airloads, and stability and control
GB894365A (en) Improvements in aeroplanes
ES67724U (es) Juguete avión planeador perfeccionado