NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Experimental aerodynamic characteristics of 120 deg included-angle cone with attached and separated 20 deg included-angle cone at Mach numbers of 2.36 and 2.70An investigation has been conducted in a unitary plan wind tunnel to determine the aerodynamic characteristics of two different size blunt 120 deg-included-angle cones behind a 20 deg-included-angle cone. Forces and moments were measured at Mach numbers of 2.36 and 2.70, longitudinal separation distances from 0 to 3.5 body diameters, lateral (side) distances from 0 to 0.50 body diameter, angles of attack of the 120 deg-included-angle cone from 0.5 deg to 22 deg, angles of attack of the 20 deg-included-angle cone from 0 deg to 180 deg, and a Reynolds number of one million per foot. Large variations in pitching-moment, normal-force, and axial-force coefficients were noted for both Mach numbers and all longitudinal distances for the 120 deg cones in the wake of a 20 deg cone.
Document ID
19730002278
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Brown, C. A., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Trescot, C. D., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Richardson, C. S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
L-8424
NASA-TM-X-2603
Accession Number
73N11005
Funding Number(s)
PROJECT: RTOP 117-07-04-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available