Suggested Topics within your search.
Suggested Topics within your search.
- Turbomachines
- Aerodynamics 80
- Blades 79
- Fluid dynamics 68
- Design and construction 39
- Rotors 36
- Compressors 35
- Vibration 24
- Air flow 22
- Turbines 21
- Airplanes 17
- Impellers 17
- Dynamics 16
- Heat 15
- Performance 15
- Transmission 15
- Mathematical models 14
- Cascades (Fluid dynamics) 13
- Gas-turbines 13
- Bearings 12
- Mathematical analysis 12
- Computer simulation 10
- Fluid mechanics 10
- Hydraulic machinery 10
- Testing 10
- Aeroelasticity 9
- Noise 9
- Numerical grid generation (Numerical analysis) 9
- Thermodynamics 9
- Unsteady flow (Aerodynamics) 9
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1
A method of designing turbomachine blades with a desirable thickness distribution for compressible flow along an arbitrary stream filament of revolution /
Published 1951Government Document Book -
2
A method of solving the direct and inverse problem of supersonic flow along arbitrary stream filaments of revolution in turbomachines /
Published 1951Government Document Book -
3
Expressions for measuring the accuracy of approximate solutions to compressible flow through cascades of blades with examples of use /
Published 1951Government Document Book -
4
Possible application of blade boundary-layer control to improvement of design and off-design performance of axial-flow turbomachines /
Published 1951Government Document Book -
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Analytical investigation of some three-dimensional flow problems in turbomachines /
Published 1952Search for the full-text version of this title in HathiTrust
Government Document Book -
8
A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial-, radial-, and mixed-flow types /
Published 1952Government Document Book -
9
Approximate design method for high-solidity blade elements in compressors and turbines /
Published 1951Government Document Book -
10
Method of analysis for compressible flow past arbitrary turbomachine blades on general surface of revolution /
Published 1951Government Document Book -
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12
Theoretical augmentation of turbine-propeller engine by compressor-inlet water injection, tail-pipe burning, and their combination /
Published 1952Government Document Book -
13
An applicational process for dynamic balancing of turbomachinery shafting
Published 1990Connect to online resource
Connect to online resource
Government Document Microfilm Book -
14
Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics /
Published 1955Government Document Book -
15
Experimental investigation of blade flutter in an annular cascade /
Published 1955Government Document Book -
16
Tabulation of mass-flow parameters for use in design of turbomachine blade rows for ratios of specific heats of 1.3 and 1.4 /
Published 1956Government Document Book -
17
Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade /
Published 1957Government Document Book -
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20
Evaluation of three methods for determining dynamic characteristics of a turbojet engine /
Published 1952Government Document Book