The N.A.C.A. CYH airfoil section / by George J. Higgins.

Format:

Book

Government document

Author/Creator:

Higgins, George J., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 240.

Technical notes / National Advisory Committee for Aeronautics ; No. 240

Language:

English

Subjects (All):

Aerofoils.

Aerodynamics.

Lift (Aerodynamics).

aerodynamics.

Physical Description:

1 online resource (4 pages, 3 unnumbered pages) : illustrations

Other Title:

National Advisory Committee for Aeronautics CYH airfoil section

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1926.

Summary:

The N.A.C.A. CYH airfoil section is described and its aerodynamic characteristics are given as tested in the N.A.C.A. variable density wind tunnel at twenty atmospheres pressure. This section has a low drag, a high maximum lift, and a small travel of center of pressure.

Notes:

Online resource, PDF version; title from title page (TRAIL, viewed May 20, 2020).

"June 1926."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

Print version record.

Other Format:

Print version: Higgins, George J. N.A.C.A. CYH airfoil section

OCLC:

1127388906