Accession Number : AD0467829


Title :   THE ZERO-LIFT FOREDRAG AND BODY BASE DRAG COEFFICIENTS OF A SERIES OF RING TAIL-STRUT-BODY CONFIGURATIONS AT MACH NUMBERS FROM 0.80 TO 4.50


Descriptive Note : Technical rept.


Corporate Author : ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL AEROBALLISTICS DIRECTORATE


Personal Author(s) : Connolly, Paul R


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/467829.pdf


Report Date : 28 May 1965


Pagination or Media Count : 39


Abstract : An investigation of the aerodynamic characteristics of a family of ring tail strut-body configurations was conducted at Mach numbers from 0.80 to 4.5. Rings varying from 1.25 to 2.50 calibers in diameter and from 0.60 to 1.50 calibers in length were tested. They were tested at various longitudinal positions and with internal expansion angles from 0 to 6 degrees. The effect of changing from circular section support struts to streamlined struts was also investigated. This report presents the zero-lift foredrag and base drag results and compares them, wherever possible, with theoretical estimates.


Descriptors :   *AERODYNAMIC CONFIGURATIONS , *SURFACE TO SURFACE MISSILES , AERODYNAMIC CHARACTERISTICS , DRAG , GUIDED MISSILE MODELS , INTERFERENCE , MODEL TESTS , OGIVES , RING WINGS , SUPERSONIC CHARACTERISTICS , SUPERSONIC FLOW , TRANSONIC CHARACTERISTICS , WIND TUNNEL MODELS


Subject Categories : Aerodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE