Achievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles / by J.C. Evvard and Lawrence R. Marcus.

Format:

Book

Government document

Author/Creator:

Evvard, John C., author.

Marcus, Lawrence R., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 2616.

Technical notes / National Advisory Committee for Aeronautics ; No. 2616

Language:

English

Subjects (All):

Supersonic nozzles--Design and construction.

Supersonic nozzles.

Wind tunnels.

Physical Description:

1 online resource (8 pages) : illustrations

Place of Publication:

Washington [D.C.] : National Advisory Committee for Aeronautics, 1952.

Summary:

Auxiliary boundary conditions were derived to assure continuity of wall curvature in applying the method of characteristics to the design of two-dimensional supersonic nozzles.

Notes:

Title from title screen (viewed March 7, 2019).

"January 1952."

"Lewis Flight Propulsion Laboratory, Cleveland, Ohio."

"[Prepared at] Lewis Flight Propulsion Laboratory ... October 16, 1951"--Page 5

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 5).

Print version record.

Other Format:

Paper version: Evvard, John C. Achievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles

OCLC:

1100474441