GB720466A - Improvements in or relating to wind tunnels - Google Patents

Improvements in or relating to wind tunnels

Info

Publication number
GB720466A
GB720466A GB3130750A GB3130750A GB720466A GB 720466 A GB720466 A GB 720466A GB 3130750 A GB3130750 A GB 3130750A GB 3130750 A GB3130750 A GB 3130750A GB 720466 A GB720466 A GB 720466A
Authority
GB
United Kingdom
Prior art keywords
section
exhaust
working
throat
engine
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
GB3130750A
Inventor
Ferdinand Basil Greatrex
Frederick Reginald Murray
Walter John Dinnie Annand
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB3130750A priority Critical patent/GB720466A/en
Publication of GB720466A publication Critical patent/GB720466A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02Wind tunnels
    • G01M9/04Details

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Testing Of Engines (AREA)

Abstract

720,466. Wind tunnels. ROLLS-ROYCE, Ltd. March 21, 1952, [Dec. 22, 1950], No. 31307/50. Class 4. The flow of working fluid through a wind tunnel is caused by the exhaust of one or more gas turbines 10 set upstream of the working section 23 of the tunnel, and consists wholly or substantially wholly of the exhaust flow from said turbines. The exhaust duct of the engine is jointed at 14 to a divergent section 15, itself jointed at 19 to section 20 having a throat 21 and leading to a working section 23 of constant or slightly divergent exhaust section 24, or, for supersonic work, a second throat. Joint 14 is shown in section in Fig. 3; glands 13a on section 13 bolted to the engine exhaust duct sliding to allow longitudinal expansion, and member 16 sliding inside members 18 and 17, the latter being secured to section 15, allowing for misalignment of the engine. Joint 19 is similar, but without provision for expansion. The throat and working sections 21 and 23 are surrounded by heat retaining panels 32 of asbestos sandwiched between aluminium plates, the inner facing plate being polished. Heaters, preferably electric, are situated between these panels and the wind tunnel itself, and are employed to raise gradually the temperature of the enclosed sections prior to starting the turbine, thus eliminating thermal distortion due to the hot exhaust. A portion of the working section and the exhaust section may be slidable on wheels, to allow easy access to the test model.
GB3130750A 1950-12-22 1950-12-22 Improvements in or relating to wind tunnels Expired GB720466A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3130750A GB720466A (en) 1950-12-22 1950-12-22 Improvements in or relating to wind tunnels

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3130750A GB720466A (en) 1950-12-22 1950-12-22 Improvements in or relating to wind tunnels

Publications (1)

Publication Number Publication Date
GB720466A true GB720466A (en) 1954-12-22

Family

ID=10321173

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3130750A Expired GB720466A (en) 1950-12-22 1950-12-22 Improvements in or relating to wind tunnels

Country Status (1)

Country Link
GB (1) GB720466A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3029635A (en) * 1956-07-09 1962-04-17 Amalgamated Growth Ind Inc High-temperature testing apparatus
CN103149237A (en) * 2013-02-18 2013-06-12 西安交通大学 Wide-Reynolds-number-range plate-fin heat exchanger heat transfer and flow performance testing apparatus
CN104280205A (en) * 2014-10-24 2015-01-14 中国人民解放军国防科学技术大学 Supersonic velocity laminar flow spraying pipe and supersonic velocity quiet wind tunnel thereof
CN108195553A (en) * 2016-12-08 2018-06-22 中国航空工业集团公司沈阳空气动力研究所 A kind of supersonic aircraft sonic boom token test measuring device
CN111912596A (en) * 2020-07-27 2020-11-10 西北工业大学 Small-sized straight-flow wind tunnel diffusion section with ultra-long fairing and annular separation-preventing net
CN114563158A (en) * 2022-04-28 2022-05-31 中国空气动力研究与发展中心超高速空气动力研究所 Controllable device that adds of shock tunnel pollution component
CN115031919A (en) * 2022-08-10 2022-09-09 中国航空工业集团公司沈阳空气动力研究所 Continuous wind tunnel two-throat channel
CN117890061A (en) * 2024-03-18 2024-04-16 百林机电科技(苏州)有限公司 Wind tunnel combined with robot and calibrated by full-automatic anemometer
CN118150105A (en) * 2024-03-13 2024-06-07 百林机电科技(苏州)有限公司 Rapid heating wind tunnel

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3029635A (en) * 1956-07-09 1962-04-17 Amalgamated Growth Ind Inc High-temperature testing apparatus
CN103149237A (en) * 2013-02-18 2013-06-12 西安交通大学 Wide-Reynolds-number-range plate-fin heat exchanger heat transfer and flow performance testing apparatus
CN104280205A (en) * 2014-10-24 2015-01-14 中国人民解放军国防科学技术大学 Supersonic velocity laminar flow spraying pipe and supersonic velocity quiet wind tunnel thereof
CN108195553A (en) * 2016-12-08 2018-06-22 中国航空工业集团公司沈阳空气动力研究所 A kind of supersonic aircraft sonic boom token test measuring device
CN111912596A (en) * 2020-07-27 2020-11-10 西北工业大学 Small-sized straight-flow wind tunnel diffusion section with ultra-long fairing and annular separation-preventing net
CN111912596B (en) * 2020-07-27 2022-06-07 西北工业大学 Small-sized straight-flow wind tunnel diffusion section with ultra-long fairing and annular separation-preventing net
CN114563158A (en) * 2022-04-28 2022-05-31 中国空气动力研究与发展中心超高速空气动力研究所 Controllable device that adds of shock tunnel pollution component
CN115031919A (en) * 2022-08-10 2022-09-09 中国航空工业集团公司沈阳空气动力研究所 Continuous wind tunnel two-throat channel
CN118150105A (en) * 2024-03-13 2024-06-07 百林机电科技(苏州)有限公司 Rapid heating wind tunnel
CN117890061A (en) * 2024-03-18 2024-04-16 百林机电科技(苏州)有限公司 Wind tunnel combined with robot and calibrated by full-automatic anemometer
CN117890061B (en) * 2024-03-18 2024-05-28 百林机电科技(苏州)有限公司 Wind tunnel combined with robot and calibrated by full-automatic anemometer

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