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The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / by Ivan E. Beckwith, Herbert W. Ridyard, and Nancy Cromer.
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- Book
- Government document
- Author/Creator:
- Beckwith, Ivan E., author.
- Ridyard, Herbert W., author.
- Cromer, Nancy, author.
- Series:
- Technical note (United States. National Advisory Committee for Aeronautics) ; 2711.
- Technical notes / National Advisory Committee for Aeronautics ; No. 2711
- Language:
- English
- Subjects (All):
- Nozzles--Fluid dynamics.
- Nozzles.
- Supersonic nozzles--Design and construction.
- Supersonic nozzles.
- Axial flow.
- Wind tunnel testing.
- Mathematical analysis.
- Physical Description:
- 1 online resource (30 pages) : illustrations
- Place of Publication:
- Washington [D.C.] : National Advisory Committee for Aeronautics, 1952.
- Summary:
- A method is given for the design of three-dimensional nozzles utilizing axisymmetric flow to produce uniform flow in a test chamber of arbitrary cross section. The method is applied to obtain the coordinates of a Mach number 10 nozzle for which a square test section is specified. Radial flow is used in a portion of the flow field to reduce the computation time. The remainder of the flow field is computed by the method of characteristics, but a simplified method is used near the axis. Tables which facilitate computation of the radial flow and the flow near the axis are included. Transition streamlines determined from the analytic expressions of Kuno Foelsch are compared with the streamlines obtained from the characteristic net of the Mach number 10 nozzle.
- Notes:
- Title from title screen (viewed March 7, 2019).
- "June 1952."
- "Langley Aeronautical Laboratory, Langley Field, Va."
- No Federal Depository Library Program (FDLP) item number.
- Includes bibliographical references (page 18).
- Print version record.
- Other Format:
- Print version: Beckwith, Ivan E. Aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section
- OCLC:
- 1100474265
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