Published June 26, 1943
| Submitted
Technical Report
Open
Water Tunnel Tests of the M7, 2.36" A.T. Rocket
- Creators
- Knapp, Robert T.
Chicago
An error occurred while generating the citation.
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.
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.Attached Files
Submitted - Water_Tunnel_Tests_of_the_M7_2.36_A.T._Rocket.pdf
Files
Water_Tunnel_Tests_of_the_M7_2.36_A.T._Rocket.pdf
Files
(7.0 MB)
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Additional details
- Alternative 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
- Eprint ID
- 61186
- Resolver ID
- CaltechAUTHORS:20151015-155247079
- National Defense Research Committee
- OEMsr-207
- Created
-
2015-10-15Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Caltech groups
- Hydrodynamics Laboratory
- Other Numbering System Name
- Hydrodynamics Laboratory
- Other Numbering System Identifier
- 47