Performance of NACA Eight-stage Axial-flow Compressor at Simulated Altitude

Performance of NACA Eight-stage Axial-flow Compressor at Simulated Altitude
Author: J. Austin King
Publisher:
Total Pages: 30
Release: 1944
Genre: Axial flow compressors
ISBN:

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An investigation has been conducted by the NACA to determine the design-performance characteristics of the NACA eight-stage axial-flow compressor and the effect of altitude on the performance. The compressor was tested at simulated altitudes of 50,000; 36,000; and 27,000 feet at rotor speeds corresponding to compressor Mach numbers of 0.80, 0.85, 0.90, and 0.95 wit varying air flow at each speed.

Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory

Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory
Author: John T. Sinnette
Publisher:
Total Pages: 74
Release: 1944
Genre: Aerofoils
ISBN:

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The NACA has conducted an investigation to determine the performance that can be obtained from a multistage axial-flow compressor based on airfoil research. A theory was developed; an eight-stage axial-flow compressor was designed, constructed, and tested.

NACA Research Memorandum

NACA Research Memorandum
Author:
Publisher:
Total Pages: 102
Release: 19??
Genre: Aerodynamics
ISBN:

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Wartime Report

Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 334
Release: 1944
Genre: Aeronautics
ISBN:

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