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GB506007A - Improvements in or relating to a method of and means for reducing surface friction between a solid and a fluid - Google Patents

Improvements in or relating to a method of and means for reducing surface friction between a solid and a fluid

Info

Publication number
GB506007A
GB506007A GB31996/37A GB3199637A GB506007A GB 506007 A GB506007 A GB 506007A GB 31996/37 A GB31996/37 A GB 31996/37A GB 3199637 A GB3199637 A GB 3199637A GB 506007 A GB506007 A GB 506007A
Authority
GB
United Kingdom
Prior art keywords
relating
fluid
solid
surface friction
reducing surface
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
GB31996/37A
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.)
HAROLD JAMES PAYN
Original Assignee
HAROLD JAMES PAYN
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 HAROLD JAMES PAYN filed Critical HAROLD JAMES PAYN
Priority to GB31996/37A priority Critical patent/GB506007A/en
Publication of GB506007A publication Critical patent/GB506007A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

506,007. Cylinders. PAYN. H. J. Nov. 20, 1937, No. 31996. [Class 7 (ii)] [Also in Group XXXIII] The exhaust gases from an aircraft engine are dicharged rearwardly through nozzle offices of contracting form disposed in a ring around the fuselage or engine nacelle as near as possible to the nose thereof. An annular noozzle 14 may be formed at the nose of an exhaust-gas collecting-ring 12 forming the leading edge of an engine cowling 11. Specifications 438,037 and 471,177, [both in Group XXXIII], are referred to.
GB31996/37A 1937-11-20 1937-11-20 Improvements in or relating to a method of and means for reducing surface friction between a solid and a fluid Expired GB506007A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB31996/37A GB506007A (en) 1937-11-20 1937-11-20 Improvements in or relating to a method of and means for reducing surface friction between a solid and a fluid

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB31996/37A GB506007A (en) 1937-11-20 1937-11-20 Improvements in or relating to a method of and means for reducing surface friction between a solid and a fluid

Publications (1)

Publication Number Publication Date
GB506007A true GB506007A (en) 1939-05-22

Family

ID=10331459

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31996/37A Expired GB506007A (en) 1937-11-20 1937-11-20 Improvements in or relating to a method of and means for reducing surface friction between a solid and a fluid

Country Status (1)

Country Link
GB (1) GB506007A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2956760A (en) * 1955-06-21 1960-10-18 John S Attinello Controllable and variable configuration effect system for aircraft
US3028129A (en) * 1957-04-08 1962-04-03 Faillie Andre Jean Stream-lined aircraft body

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2956760A (en) * 1955-06-21 1960-10-18 John S Attinello Controllable and variable configuration effect system for aircraft
US3028129A (en) * 1957-04-08 1962-04-03 Faillie Andre Jean Stream-lined aircraft body

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