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Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory
"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. The performance of the compressor was determined for speeds from 5000 to 14,000 r.p.m with varying air flow at each speed" (p. 81).
Date:
August 1, 1944
Creator:
Sinnette, John T., Jr.; Schey, Oscar W. & King, J. Austin
System:
The UNT Digital Library
An Interim Report on the Stability and Control of Tailless Airplanes
Problems relating to the stability and control of tailless airplanes are discussed in consideration of contemporary experience and practice.
Date:
August 19, 1944
Creator:
Donlan, Charles J.
System:
The UNT Digital Library
An Interim Report on the Stability and Control of Tailless Airplanes
Problems relating to the stability and control of tailless airplanes are discussed in consideration of contemporary experience and practice.
Date:
August 19, 1944
Creator:
Donlan, Charles J.
System:
The UNT Digital Library