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Static Force Coefficients of the Basic Finner Missile in Fully Wetted Flow

Kermeen, R. W. (1957) Static Force Coefficients of the Basic Finner Missile in Fully Wetted Flow. California Institute of Technology , Pasadena, CA. (Unpublished) http://resolver.caltech.edu/CaltechAUTHORS:20150526-132445332

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Abstract

The results of force tests of models of the Basic Finner missile configuration in fully wetted flow in the High Speed Water Tunnel are presented. The static lift, pitching moment and drag were measured for angles of attack up to 14 degrees and for Reynolds numbers from 0.7 to 8.5 x 10^6. The results of these tests performed on the static force balance are in good agreement with coefficients determined from free flight drag studies in the Controlled Atmosphere Launching Tank and at the U. S. Naval Ordnance Test Station, Pasadena.


Item Type:Report or Paper (Technical Report)
Additional Information:Department of the Navy Bureau of Ordnance Contract NOrd-16200 Task 1. Report No. E-73.2.
Group:Hydrodynamics Laboratory
Funders:
Funding AgencyGrant Number
Department of the Navy Bureau of OrdnanceNOrd-16200
Record Number:CaltechAUTHORS:20150526-132445332
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20150526-132445332
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:57813
Collection:CaltechAUTHORS
Deposited By: Kristin Buxton
Deposited On:27 May 2015 19:06
Last Modified:27 May 2015 19:06

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