GB219951A - Aircraft with low transverse stability or transverse instability - Google Patents

Aircraft with low transverse stability or transverse instability

Info

Publication number
GB219951A
GB219951A GB14542/24A GB1454224A GB219951A GB 219951 A GB219951 A GB 219951A GB 14542/24 A GB14542/24 A GB 14542/24A GB 1454224 A GB1454224 A GB 1454224A GB 219951 A GB219951 A GB 219951A
Authority
GB
United Kingdom
Prior art keywords
transverse
instability
low
wings
aircraft
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
GB14542/24A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB219951A publication Critical patent/GB219951A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)

Abstract

219,951. Rohrbach, A., (Assignee ot Rohrbach Metall-Flugzeugbau Ges.). Aug. 3, 1923, [Convention date]. Void [Published under Sect. 91 of the Act]. Planes, arrangement of.-To increase manoeuvrability, an aeroplane is given a low statical transverse stability or instability by setting the wings at a dihedral angle of more than 3‹. Biplanes and multiplanes may have all the wings set at the same dihedral angle or the top wings may only have a slight dihedral.
GB14542/24A 1923-08-03 1924-06-16 Aircraft with low transverse stability or transverse instability Expired GB219951A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE219951X 1923-08-03

Publications (1)

Publication Number Publication Date
GB219951A true GB219951A (en) 1925-04-30

Family

ID=5832158

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14542/24A Expired GB219951A (en) 1923-08-03 1924-06-16 Aircraft with low transverse stability or transverse instability

Country Status (1)

Country Link
GB (1) GB219951A (en)

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