Transonic Investigation of an Axial-flow Compressor Rotor with a Hub-tip Ratio of 0.75 and Blades Having NACA A(sub 2)i(sub 8b) Mean Lines
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Bernot, Peter T↗
Engineering topics
Savage, Melvyn
Publications and source records attributed to Savage, Melvyn.
Investigation of a High-performance Axial-flow Compressor Transonic Inlet Rotor Designed for 37.5 Pounds Per Second Per Square Foot of Frontal Area : Detailed Blade-element Performance
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Felix, A Richard↗
Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading
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Erwin, John R↗
Investigation of a Three-stage Transonic Research Axial-flow Compressor : Aerodynamic Design and Overall Performance
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Savage, Melvyn↗
High-speed Cascade Tests of a Blade Section Designed for Typical Hub Conditions of High-flow Transonic Rotors
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Savage, Melvyn↗
Analysis of aerodynamic blade-loading-limit parameters for NACA 65-(C(sub zeta(sub o)) A(sub 10)) 10 compressor-blade sections at low speeds
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Savage, Melvyn↗
Investigation of a High-performance Axial-flow Compressor Transonic Inlet Rotor Designed for 37.5 Pounds Per Second Per Square Foot of Frontal Area : Aerodynamic Design and Overall Performance
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Savage, Melvyn↗
Low-speed Cascade Tests of Two 45 Degree Swept Compressor Blades with Constant Spanwise Loading
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Beatty, Loren A↗
Investigation of an Axial-flow Compressor Rotor Having NACA High-speed Blade Sections (a(sub 2)i(sub 8b) Series) at Mean Radius Relative Inlet Mach Numbers up to 1.13
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Savage, Melvyn↗
Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading
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Erwin, John R↗
Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients
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Beatty, Loren A↗
A Technique Applicable to the Aerodynamic Design of Inducer-type Multistage Axial-flow Compressors
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Savage, Melvyn↗
Analysis of the effects of design pressure ratio per stage and off-design efficiency on the operating range of multistage axial-flow compressors
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COMPRESSORS, AXIAL↗