SU494626A1 - Heat flow measurement method - Google Patents
Heat flow measurement methodInfo
- Publication number
- SU494626A1 SU494626A1 SU1937886A SU1937886A SU494626A1 SU 494626 A1 SU494626 A1 SU 494626A1 SU 1937886 A SU1937886 A SU 1937886A SU 1937886 A SU1937886 A SU 1937886A SU 494626 A1 SU494626 A1 SU 494626A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- measurement method
- heat flow
- flow measurement
- heat
- heat flows
- Prior art date
Links
Landscapes
- Investigating Or Analyzing Materials Using Thermal Means (AREA)
- Measuring Temperature Or Quantity Of Heat (AREA)
Description
(54) СПОСОБ ИЗМЕРЕНИЯ ТЕПЛОВЫХ ПОТОКОВ(54) METHOD FOR MEASURING HEAT FLOWS
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1937886A SU494626A1 (en) | 1973-06-28 | 1973-06-28 | Heat flow measurement method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1937886A SU494626A1 (en) | 1973-06-28 | 1973-06-28 | Heat flow measurement method |
Publications (1)
Publication Number | Publication Date |
---|---|
SU494626A1 true SU494626A1 (en) | 1975-12-05 |
Family
ID=20558207
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1937886A SU494626A1 (en) | 1973-06-28 | 1973-06-28 | Heat flow measurement method |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU494626A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103398835B (en) * | 2013-08-21 | 2016-01-06 | 中国人民解放军国防科学技术大学 | Based on gaseous film control transient heat flow test macro and the method for hypersonic gun wind tunnel |
-
1973
- 1973-06-28 SU SU1937886A patent/SU494626A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103398835B (en) * | 2013-08-21 | 2016-01-06 | 中国人民解放军国防科学技术大学 | Based on gaseous film control transient heat flow test macro and the method for hypersonic gun wind tunnel |
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