Knapp, Robert T. (1943) Water Tunnel Tests of the M6, 2.36" A.T. Rocket. California Institute of Technology , Pasadena, CA. (Unpublished) https://resolver.caltech.edu/CaltechAUTHORS:20151014-125552476
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Abstract
This report covers Water Tunnel tests of a 2.36" rocket projectile with three types of shroud ring tail. Two of the tails are attached by channel section supporting fins to a stepped nozzle, the fins on one of them being stepped to fit the nozzle contour. The third tail has a streamlined nozzle with smooth supporting fins and shroud ring. The results are given of tests with different shroud lengths on the ring tails with the channel section supporting fins.
| Item Type: | Report or Paper (Technical Report) | ||||
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| Alternate Title: | Memorandum on Water Tunnel Tests of the M-6, 2.36" A. T. Rocket Showing Comparison of Performance with the Conical Pointed Nose Combined with Three Types of Shroud Ring Tail and with Shroud Rings of Various Lengths | ||||
| Additional Information: | Office of scientific Research & Development National Defense Research Committee. Division Six-Section 6.1. Section No. 6.1-sr-207-920. HML Rep. No. ND-11.4. | ||||
| Group: | Hydrodynamics Laboratory | ||||
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| Record Number: | CaltechAUTHORS:20151014-125552476 | ||||
| Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20151014-125552476 | ||||
| Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | ||||
| ID Code: | 61103 | ||||
| Collection: | CaltechAUTHORS | ||||
| Deposited By: | INVALID USER | ||||
| Deposited On: | 14 Oct 2015 20:00 | ||||
| Last Modified: | 03 Oct 2019 09:04 |
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