Preliminary Transient Performance Data on the J73 Turbojet Engine, 3: Altitude, 45,000 Feet Page: 5 of 96
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NACA RM SE53F30
scale on all traces is a circular arc. In obtaining the rate of change
of any variable or in calculating elapsed time, this curvature must be
Lewis Flight Propulsion Laboratory
National Advisory Committee for Aeronautics
Cleveland, Ohio, July 1, 1953
1. Sobolewski, Adam E., and Lubick, Robert J.: Preliminary Transient
Performance Data on the J73 Turbojet Engine. I - Altitude, Sea
Level and 15,000 Feet. NACA RM SE53F22, 1953.
2. Lubick, Robert J., and Sobolewski., Adam E.: Preliminary Transient
Performance Data on the J73 Turbojet Engine. II - Altitude,
35,000 Feet. NACA RM SE53F29, 1953.
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McAulay, John E. & Wallner, Lewis E. Preliminary Transient Performance Data on the J73 Turbojet Engine, 3: Altitude, 45,000 Feet, report, July 16, 1953; (https://digital.library.unt.edu/ark:/67531/metadc65444/m1/5/: accessed March 24, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.