The Aerodynamic Design and Calibration of an Asymmetric Variable Mach Number Nozzle with a Sliding Block for the Mach Number Range 1.27 to 2.75.
- Author
- Burbank, Paige B
- Published
- April 1953.
- Physical Description
- 1 electronic document
- Additional Creators
- Byrne, Robert W
Online Version
- hdl.handle.net , Connect to this object online.
- Restrictions on Access
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary
- A method of designing as asymmetric, fixed geometry, variable Mach number nozzle has been developed by using the method of characteristics. A small nozzle conforming to the analytically determined ordinates was constructed and calibrated over a range of Mach numbers extending from 1.27 to 2.75. The results show the variation in Mach number to be plus or minus 0.01 or less and in the flow direction to be plus or minus 0.2 degrees within the test section. The range of Mach numbers from 1.27 to 2.75 was obtained by translating the lower block in a straight line parallel to the test-section center line for a distance of 2.17 test-section heights.
- Collection
- NASA Technical Reports Server (NTRS) Collection.
- Note
- Document ID: 19930083639.
Accession ID: 93R12929.
NACA-TN-2921. - Terms of Use and Reproduction
- No Copyright.
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