Suggested Topics within your search.
Suggested Topics within your search.
- Axial flow
- Air flow 16
- Blades 15
- Compressors 13
- Aerodynamics, Supersonic 12
- Fans (Machinery) 11
- Fluid dynamics 11
- Aerodynamics 9
- Airplanes 9
- Mathematical analysis 9
- Turbines 9
- Charts, diagrams, etc 8
- Jets 8
- Design and construction 7
- Mathematics 7
- Body of revolution 6
- Nozzles 6
- Turbomachines 6
- Aerofoils 5
- Computational fluid dynamics 5
- Impellers 5
- Supersonic nozzles 5
- Axial flow compressors 4
- Boundary layer 4
- Cascades (Fluid dynamics) 4
- Motors 4
- Performance 4
- Cylinders 3
- Laminar flow 3
- Mach number 3
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1
Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams /
Published 1981Online Access
Online Access
Government Document eBook -
2
Two axial-symmetry solutions for incompressible flow through a centrifugal compressor with and without inducer vanes /
Published 1951Government Document Book -
3
Linearized supersonic axially symmetric flow about open-nosed bodies obtained by use of stream function /
Published 1950Government Document Book -
4
An analysis of base pressure at supersonic velocities and comparison with experiment /
Published 1950Government Document Book -
5
An analysis of flow in rotating passage of large radial-inlet centrifugal compressor at tip speed of 700 feet per second /
Published 1951Government Document Book -
6
Possible application of blade boundary-layer control to improvement of design and off-design performance of axial-flow turbomachines /
Published 1951Government Document Book -
7
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
Influence of wall boundary layer upon the performance of an axial-flow fan rotor /
Published 1951Search for the full-text version of this title in HathiTrust
Government Document Book -
9
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10
Approximate design method for high-solidity blade elements in compressors and turbines /
Published 1951Government Document Book -
11
Effect of heat and power extraction on turbojet-engine performance. : 2 - Effect of compressor-outlet air bleed for specific modes of engine operation /
Published 1950Government Document Book -
12
Turning-angle design rules for constant-thickness circular-arc inlet guide vanes in axial annular flow /
Published 1950Government Document Book -
13
Compressibility correction for turning angles of axial-flow inlet guide vanes /
Published 1950Government Document Book -
14
The linearized characteristics method and its application to practical nonlinear supersonic problems /
Published 1951Government Document Book -
15
Minimum wave drag of bodies of revolution with a cylindrical center section /
Published 1951Government Document Book -
16
An approximate solution for axially symmetric flow over a cone with an attached shock wave /
Published 1955Government Document Book -
17
Three-dimensional supersonic nozzles and inlets of arbitrary exit cross section /
Published 1952Government Document Book -
18
One-dimensional analysis of choked-flow turbines /
Published 1952Search for the full-text version of this title in HathiTrust
Government Document Book -
19
A note on secondary flow in rotating radial channels /
Published 1953Search for the full-text version of this title in HathiTrust
Government Document Book -
20