The characteristics of the N.A.C.A. 97, Clark Y, and N.A.C.A.-M6 airfoils with particular reference to the angle of attack / 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) ; 270.

Technical notes / National Advisory Committee for Aeronautics ; No. 270

Language:

English

Subjects (All):

Aerofoils.

Airplanes--Design and construction.

Airplanes.

Wind tunnels.

Physical Description:

1 online resource (4 pages, 8 unnumbered pages) : illustrations.

Other Title:

Characteristics of the National Advisory Committee for Aeronautics 97, Clark Y, and National Advisory Committee for Aeronautics-M6 airfoils with particular reference to the angle of attack

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1927.

Summary:

This note gives the aerodynamic characteristics of the N.A.C.A. 97, Clark Y, and N.A.C.A.-M6 airfoil sections as determined in the variable density wind tunnel al Langley Field, Virginia. Particular attention is called to the relation of the characteristics to the angle of attack in their use in airplane design.

Notes:

Description based on online resource, PDF version; title from title page (TRAIL, viewed June 2, 2020).

"December 1927."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

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

Other Format:

Print version: Higgins, George J. The characteristics of the N.A.C.A. 97, Clark Y, and N.A.C.A.-M6 airfoils with particular reference to the angle of attack

OCLC:

1127388938