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Interference of wing and fuselage from tests of 30 combinations with triangular and elliptical fuselages in the NACA variable-density tunnel

Author: Albert Sherman; United States. National Advisory Committee for Aeronautics.; Langley Aeronautical Laboratory.
Publisher: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series: Technical note (United States. National Advisory Committee for Aeronautics), no. 1272.
Edition/Format:   Book : National government publication : EnglishView all editions and formats
Database:WorldCat
Summary:
Tests of 12 wing-fuselage combinations employing triangluar and 18 employing elliptical fuselages were made in the NACA variable-density tunnel as a part of a program to investigate at large values of Reynolds number the aerodynamic effects of wing-fuselage interference. This program is outined in NACA Report no. 540, which contains the test results for 209 combinations, 202 with round and 7 with rectangular  Read more...
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Details

Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: Albert Sherman; United States. National Advisory Committee for Aeronautics.; Langley Aeronautical Laboratory.
OCLC Number: 38208015
Notes: "May 1947."
NACA TN No. 1272.
Description: 12, [16] p. : ill., tables ; 27 cm.
Series Title: Technical note (United States. National Advisory Committee for Aeronautics), no. 1272.
Responsibility: by Albert Sherman.

Abstract:

Tests of 12 wing-fuselage combinations employing triangluar and 18 employing elliptical fuselages were made in the NACA variable-density tunnel as a part of a program to investigate at large values of Reynolds number the aerodynamic effects of wing-fuselage interference. This program is outined in NACA Report no. 540, which contains the test results for 209 combinations, 202 with round and 7 with rectangular fuselages, comprising the basic part of the wing-fuselage interference investigation.

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