Knapp, Robert T. (1943) Water Tunnel Tests of the M7, 2.36" A.T. Rocket. California Institute of Technology , Pasadena, CA. (Unpublished) https://resolver.caltech.edu/CaltechAUTHORS:20151015-155247079
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Abstract
This report covers water tunnel tests of a 2.36" rocket projectile with several variations in profile of nose and with two types of tail; a folding fin tail and a fixed shroud ring tail. The hydrodynamic forces, drag, cross wind force, and moment acting on the projectile, were measured and the locations of the center-of- pressure were calculated for the various combinations of noses and tails and at various velocities and yaw angles.
| Item Type: | Report or Paper (Technical Report) | ||||
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| Alternate Title: | Memorandum on Water Tunnel Tests of the M-7, 2.36" A. T. Rocket Showing Comparison of Performance with a Folding Fin Tail A Shroud Ring Tali Two Hemispherical Ogive Noses of Different Profile and a Conical Pointed Nose | ||||
| Additional Information: | Office of Scientific Research & Development National Defense Research Committee. Division Six-Section 6.1. Section No 6.1-Sr-207-276. ND-11.3. | ||||
| Group: | Hydrodynamics Laboratory | ||||
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| Record Number: | CaltechAUTHORS:20151015-155247079 | ||||
| Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20151015-155247079 | ||||
| Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | ||||
| ID Code: | 61186 | ||||
| Collection: | CaltechAUTHORS | ||||
| Deposited By: | INVALID USER | ||||
| Deposited On: | 15 Oct 2015 23:14 | ||||
| Last Modified: | 03 Oct 2019 09:05 |
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