WADC-TR-53-114
- Version
- 165 Downloads
- 43.02 MB File Size
- 1 File Count
- March 7, 2017 Create Date
- March 7, 2017 Last Updated
Ohio State University Research Foundation - Methods of Controlling Temperature Rise in Airborne Compartments at Supersonic Velocities with and Without Internal Heat Generation

Thig report 1B eoneeræa v1th presentation of the infomation de- veloped In an Investigation with the ±Jective of studying methods of cooling airborne but specifically intended produce data for controlling the temperature rise of electronic echanical control cæponents in ruået Installations. only Sections I 11 are conceræd vith analyges assuming Bteady-state thermal operation, vh11e Sections 111 through XI end Appendix 111 on fuel tempera— ture rise in flight concerned Vltb methods of analysis ana results obtained in the study Of transient thermal latter approach hag been chosen because when operating under constant environæntal condi- Clone conducive to high heat gain, fev equipnents vould reach thermal equilibrium in less tvo hours, vhich has been ooneidered ae a reason- ably long operating ti.æ for the specified applications consideration. The reductions In size and of insulation or cooling apparatus, realized by for urminal temperatures to be reached in •the transient state, rather than to be maintained in the under terminal environæntal conditions, are substantial, as indicated repeatedly In thie report. It hag been intention in preparing this N•port to present in each section a phage Of study as a self-contained unit since ele variety of aspects covered in the report has not been found to lend itBe1f reedlly to joint Bunarization. Therefore, the gunary presented in each section after the Introductory remarks 1B intended to provide indication of anaaysee, data, cone1ue10n3, degign procedures, etc. contained In that particular sec— tion. Throughout the report methods of calculations and are emphasized since it intended to provide the necessary information that •ould enable the to cope vith qpeclfic problems of similar nature In vhich are defined. Because of the number of their possible cæbinatione fev unconditional recæændatione are pre— sented. Instead an made to develop In each section the necessary criteria for the election of each of limiting temperature rise, as summarized in Section XI.
| File | Action |
|---|---|
| WADC-TR-53-114 Methods of Controlling Temperature Rise in Airborne Compartments at Supersonic Velocities with and.pdf | Download |

Comment On This Post