Interference of wing and fuselage from tests of 17 combinations in the N.A.C.A. variable-density tunnel combinations with special junctures / by Albert Sherman.

Format:

Book

Government document

Author/Creator:

Sherman, Albert, author.

Contributor:

United States. National Advisory Committee for Aeronautics, issuing body.

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 641.

Technical note / National Advisory Committee for Aeronautics ; No. 641

Language:

English

Subjects (All):

Airplanes--Wings--Testing.

Airplanes.

Airplanes--Fuselage--Testing.

Interference (Aerodynamics).

Wind tunnel testing.

Physical Description:

1 online resource (14 pages, 8 unnumbered pages) : illustrations.

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1938.

Summary:

As part of the wing-fuselage interferences investigation in progress in the N.A.C.A. variable-density wind tunnel, a method of eliminating the interference burble associated with critical midwing combinations was investigated. The interference burble of the critical midewing combination was shown to respond to modifications at the nose of the juncture and to be entirely suppressed with little or no adverse effect on the high-speed drag by special leading-edge fillets.

Notes:

Title from title screen (viewed June 18, 2020).

"March, 1938."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 12).

Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.

Other Format:

Print version: Sherman, Albert Interference of wing and fuselage from tests of 17 combinations in the N.A.C.A. variable-density tunnel combinations with special junctures

OCLC:

1159597652