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| 040 | ⊔ | ⊔ | ‡aLHL ‡beng ‡cLHL ‡dLHL ‡dOCLCO ‡dOCLCQ ‡dOCLCF ‡dTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/46-2:70-154/Volume IV |
| 088 | ⊔ | ⊔ | ‡aAFFDL TR 70-154/V.4 |
| 100 | 1 | ⊔ | ‡aFricke, L. B., ‡eauthor. |
| 245 | 1 | 2 | ‡aA wind tunnel investigation of jets exhausting into a crossflow. ‡nVolume 4, ‡pAdditional data for three-jet configuration / ‡cL.B. Fricke, P.T. Wooler, H. Ziegler. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, ‡c1970. |
| 300 | ⊔ | ⊔ | ‡avi, 191 pages : ‡billustrations, figures ; ‡c28 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.). Technical report ; ‡vAFFDL TR 70-154/Volume IV |
| 500 | ⊔ | ⊔ | ‡a"This report presents the results of Contract F33615-69-C-1602, Project No. 698BT." |
| 500 | ⊔ | ⊔ | ‡a"Northrop Corporation, Aircraft Division. |
| 500 | ⊔ | ⊔ | ‡a"December 1970." |
| 520 | ⊔ | ⊔ | ‡aA low speed wind tunnel test of a four-foot diameter circular plate model was conducted to determine surface static pressure distributions; jet paths, and jet decay characteristics in the presence of a crossflow. Data were obtained for a one-jet configuration with the jet exiting at a number of angles to the plate and at various velocity ratios and sideslip angles. The report is the second of four volumes. The test model, instrumentation, test procedure, and reduction and accuracy of the test data were discussed in Volume 1. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 583 | 1 | ⊔ | ‡awill digitize ‡c20200923 ‡zQueued for digitization ‡cSeptember 23, 2020 ‡5miu ‡2pda |
| 650 | ⊔ | 0 | ‡aNozzles ‡xFluid dynamics. |
| 650 | ⊔ | 0 | ‡aWind tunnel models. |
| 650 | ⊔ | 0 | ‡aPlates (Engineering) |
| 650 | ⊔ | 0 | ‡aVertically rising aircraft. |
| 700 | 1 | ⊔ | ‡aZiegler, Henry. ‡eauthor. |
| 700 | 1 | ⊔ | ‡aWooler, Peter T., ‡eauthor. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡eissuing agency. |
| 710 | 2 | ⊔ | ‡aNorthrop Corporation. ‡bAircraft Division, ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
| 899 | ⊔ | ⊔ | ‡a39015095328822 ‡cVolume IV (r: AFFDL-TR-70-154) |
| CID | ⊔ | ⊔ | ‡a102856160 |
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| DAT | 1 | ⊔ | ‡a20230928062550.0 ‡b2024-06-09T17:31:53Z |
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