Contents: Determination of the weight of an empty aircraft by methods of mathematical statistics; Certain results of the experimental investigation of airfoil compressor cascades with blades of small elongation; Determination of the border of stable operation of stages of an axial compressor by the calculation method; Influence of the frequency of application stress on characteristics of the strength of Aluminum Alloy B95.
Aircraft Building and Technology of the Air Fleet, Number 7, 1966 (Selected Articles)
1968
46 pages
Report
No indication
English
Aircraft , Hydraulic & Pneumatic Equipment , Iron & Iron Alloys , Jet & Gas Turbine Engines , Jet transport planes , Compressor blades , Aluminum alloys , Weight , Performance(Engineering) , Stresses , Statistical analysis , Airfoils , Cascade structures , Strength , Axial-flow compressors , USSR , Aluminum alloy 1.5Cu 2.1Mg 5.8Zn , Translations , Aluminum alloy B95
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