SU1828694A3 - Set study of flying models - Google Patents
Set study of flying modelsInfo
- Publication number
- SU1828694A3 SU1828694A3 SU4946538/23A SU4946538A SU1828694A3 SU 1828694 A3 SU1828694 A3 SU 1828694A3 SU 4946538/23 A SU4946538/23 A SU 4946538/23A SU 4946538 A SU4946538 A SU 4946538A SU 1828694 A3 SU1828694 A3 SU 1828694A3
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- strain
- gauge balance
- flying models
- study
- model
- Prior art date
Links
Landscapes
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
FIELD: experimental aerodynamics. SUBSTANCE: set for study of flying models consists of strain-gauge balance 4, holder 1 with lock 7 enclosed in fairing 3, pipe lines 8 and 9 for feeding the compressed air to model 2, bellows 10 located beyond model 2 and strain-gauge balance 4 and upright 6 connected with strain-gauge balance 4 by means of eccentric unit 5. EFFECT: extended experimental capabilities. 2 dwg
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4946538/23A SU1828694A3 (en) | 1991-06-20 | 1991-06-20 | Set study of flying models |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4946538/23A SU1828694A3 (en) | 1991-06-20 | 1991-06-20 | Set study of flying models |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1828694A3 true SU1828694A3 (en) | 1996-02-20 |
Family
ID=60537420
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4946538/23A SU1828694A3 (en) | 1991-06-20 | 1991-06-20 | Set study of flying models |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1828694A3 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110705157A (en) * | 2019-03-19 | 2020-01-17 | 北京理工大学 | Rectifying cover similar structure extrapolation correction method based on scaling model |
CN110717289A (en) * | 2019-03-19 | 2020-01-21 | 北京理工大学 | Carrier rocket radome acoustic vibration test scaling model |
CN116399548A (en) * | 2023-06-08 | 2023-07-07 | 中国空气动力研究与发展中心高速空气动力研究所 | Air inlet channel inner surface aerodynamic characteristic measurement test device and installation and test method thereof |
-
1991
- 1991-06-20 SU SU4946538/23A patent/SU1828694A3/en active
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110705157A (en) * | 2019-03-19 | 2020-01-17 | 北京理工大学 | Rectifying cover similar structure extrapolation correction method based on scaling model |
CN110717289A (en) * | 2019-03-19 | 2020-01-21 | 北京理工大学 | Carrier rocket radome acoustic vibration test scaling model |
CN110717289B (en) * | 2019-03-19 | 2021-02-19 | 北京理工大学 | Method for constructing scaling model for sound vibration test of carrier rocket fairing |
CN116399548A (en) * | 2023-06-08 | 2023-07-07 | 中国空气动力研究与发展中心高速空气动力研究所 | Air inlet channel inner surface aerodynamic characteristic measurement test device and installation and test method thereof |
CN116399548B (en) * | 2023-06-08 | 2023-08-11 | 中国空气动力研究与发展中心高速空气动力研究所 | Air inlet channel inner surface aerodynamic characteristic measurement test device and installation and test method thereof |
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