JPS63146739U - - Google Patents

Info

Publication number
JPS63146739U
JPS63146739U JP3839687U JP3839687U JPS63146739U JP S63146739 U JPS63146739 U JP S63146739U JP 3839687 U JP3839687 U JP 3839687U JP 3839687 U JP3839687 U JP 3839687U JP S63146739 U JPS63146739 U JP S63146739U
Authority
JP
Japan
Prior art keywords
gas
wind tunnel
blowout tube
aircraft model
tube
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.)
Granted
Application number
JP3839687U
Other languages
Japanese (ja)
Other versions
JPH0439556Y2 (en
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 filed Critical
Priority to JP3839687U priority Critical patent/JPH0439556Y2/ja
Publication of JPS63146739U publication Critical patent/JPS63146739U/ja
Application granted granted Critical
Publication of JPH0439556Y2 publication Critical patent/JPH0439556Y2/ja
Expired legal-status Critical Current

Links

Landscapes

  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は、本考案の一実施例の説明図、第2図
はマイクロバースト中を飛行する航空機の経路を
示す説明図である。 図面中、1は高圧ガス吹出筒、2は高圧ガス源
、3はレール、4は板、5は航空機模型、6は内
蔵天秤、7は模型支持装置、をそれぞれ示す。
FIG. 1 is an explanatory diagram of an embodiment of the present invention, and FIG. 2 is an explanatory diagram showing the path of an aircraft flying during a microburst. In the drawings, 1 is a high-pressure gas blow-off tube, 2 is a high-pressure gas source, 3 is a rail, 4 is a plate, 5 is an aircraft model, 6 is a built-in balance, and 7 is a model support device.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ガス圧力源に連通され風洞内に開口し風洞気流
を横切つてガスを吹出すガス吹出筒、同ガス吹出
筒から吹出されるガス流中におかれた航空機模型
、及び上記航空機模型の上記ガス吹出筒の開口と
反対側に配設された板からなることを特徴とする
風洞におけるマイクロバースト試験装置。
A gas blowout tube that is connected to a gas pressure source and opens in a wind tunnel and blows out gas across the wind tunnel airflow, an aircraft model placed in the gas flow blown out from the gas blowout tube, and the above-mentioned gas of the aircraft model. A microburst test device in a wind tunnel characterized by consisting of a plate placed on the opposite side of the opening of a blowout tube.
JP3839687U 1987-03-18 1987-03-18 Expired JPH0439556Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3839687U JPH0439556Y2 (en) 1987-03-18 1987-03-18

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3839687U JPH0439556Y2 (en) 1987-03-18 1987-03-18

Publications (2)

Publication Number Publication Date
JPS63146739U true JPS63146739U (en) 1988-09-28
JPH0439556Y2 JPH0439556Y2 (en) 1992-09-16

Family

ID=30850600

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3839687U Expired JPH0439556Y2 (en) 1987-03-18 1987-03-18

Country Status (1)

Country Link
JP (1) JPH0439556Y2 (en)

Also Published As

Publication number Publication date
JPH0439556Y2 (en) 1992-09-16

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