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Journal Articles

An Experiment on Compressible-Flow Perturbations

T. A. d’Ews Thomson, R. E. Meyer
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. March 1959, 26(1): 114–119.
https://doi.org/10.1115/1.4011931
Published Online: June 23, 2021
View Article titled, An Experiment on Compressible-Flow Perturbations
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Topics: Compressible flow, Flow (Dynamics), Mach number, Nozzles, Pressure gradient, Wind tunnels
Journal Articles

Theory of Flight of the Sounding Rocket

V. C. Liu
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. March 1959, 26(1): 127–129.
https://doi.org/10.1115/1.4011934
Published Online: June 23, 2021
View Article titled, Theory of Flight of the Sounding Rocket
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Topics: Depth sounding, Flight, Rockets, Density, Drag (Fluid dynamics), Equations of motion, Mach number
Journal Articles

On the Thickness of Normal Shock Waves in a Perfect Gas

A. H. Shapiro, S. J. Kline
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. June 1954, 21(2): 185–192.
https://doi.org/10.1115/1.4010862
Published Online: June 4, 2021
View Article titled, On the Thickness of Normal Shock Waves in a Perfect Gas
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Topics: Boundary layers, Gases, Mach number, Prandtl number, Relaxation (Physics), Reynolds number, Shock (Mechanics), Shock waves, Temperature, Thermal conductivity
Journal Articles

Heat-Transfer Measurements in an Inexpensive Supersonic Wind Tunnel: 2—Results for a Laminar Boundary Layer Based on a Two-Dimensional Flow Model

Joseph Kaye, G. A. Brown
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. September 1955, 22(3): 297–304.
https://doi.org/10.1115/1.4011076
Published Online: June 4, 2021
View Article titled, Heat-Transfer Measurements in an Inexpensive Supersonic Wind Tunnel: 2—Results for a Laminar Boundary Layer Based on a Two-Dimensional Flow Model
Open the PDF for Heat-Transfer Measurements in an Inexpensive Supersonic Wind Tunnel: 2—Results for a Laminar Boundary Layer Based on a Two-Dimensional Flow Model in another window
Topics: Boundary layers, Flow (Dynamics), Heat transfer, Wind tunnels, Supersonic flow, Reynolds number, Entrance region, Flat plates, Mach number
Journal Articles

Heat-Transfer Measurements in an Inexpensive Supersonic Wind Tunnel: 1—Apparatus and Results for a Laminar Boundary Layer Based on a Simple One-Dimensional Flow Model

Joseph Kaye, J. H. Keenan, G. A. Brown, R. H. Shoulberg
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. September 1955, 22(3): 289–296.
https://doi.org/10.1115/1.4011075
Published Online: June 4, 2021
View Article titled, Heat-Transfer Measurements in an Inexpensive Supersonic Wind Tunnel: 1—Apparatus and Results for a Laminar Boundary Layer Based on a Simple One-Dimensional Flow Model
Open the PDF for Heat-Transfer Measurements in an Inexpensive Supersonic Wind Tunnel: 1—Apparatus and Results for a Laminar Boundary Layer Based on a Simple One-Dimensional Flow Model in another window
Topics: Boundary layers, Flow (Dynamics), Heat transfer, Wind tunnels, Reynolds number, Boundary layer turbulence, Laminar flow, Mach number
Journal Articles

Supersonic Flow With Variable Specific Heat

F. P. Durham
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. March 1952, 19(1): 57–62.
https://doi.org/10.1115/1.4010407
Published Online: April 7, 2021
View Article titled, Supersonic Flow With Variable Specific Heat
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Topics: Specific heat, Supersonic flow, Shock waves, Temperature, Density, Equations of state, Flow (Dynamics), High pressure (Physics), Mach number, Pressure
Journal Articles

Measurement of Recovery Factors and Friction Coefficients for Supersonic Flow of Air in a Tube: 2—Results Based on a Two-Dimensional Flow Model for Entrance Region

J. Kaye, T. Y. Toong, R. H. Shoulberg
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. June 1952, 19(2): 185–194.
https://doi.org/10.1115/1.4010445
Published Online: April 7, 2021
View Article titled, Measurement of Recovery Factors and Friction Coefficients for Supersonic Flow of Air in a Tube: 2—Results Based on a Two-Dimensional Flow Model for Entrance Region
Open the PDF for Measurement of Recovery Factors and Friction Coefficients for Supersonic Flow of Air in a Tube: 2—Results Based on a Two-Dimensional Flow Model for Entrance Region in another window
Topics: Entrance region, Flow (Dynamics), Friction, Supersonic flow, Boundary layers, Boundary layer turbulence, Flat plates, Fluids, Heat transfer, Mach number
Journal Articles

Measurement of Recovery Factors and Friction Coefficients for Supersonic Flow of Air in a Tube: 1—Apparatus, Data, and Results Based on a Simple One-Dimensional Flow Model

J. Kaye, J. H. Keenan, K. K. Klingensmith, G. M. Ketchum, T. Y. Toong
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. March 1952, 19(1): 77–96.
https://doi.org/10.1115/1.4010410
Published Online: April 7, 2021
View Article titled, Measurement of Recovery Factors and Friction Coefficients for Supersonic Flow of Air in a Tube: 1—Apparatus, Data, and Results Based on a Simple One-Dimensional Flow Model
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Topics: Flow (Dynamics), Friction, Supersonic flow, Boundary layers, Heat transfer, Mach number, Reynolds number, Wall temperature, Pressure, Temperature distribution
Journal Articles

Some Experiments on the Interaction of Shock Waves With Boundary Layers on a Flat Plate

F. W. Barry, A. H. Shapiro, E. P. Neumann
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. June 1950, 17(2): 126–131.
https://doi.org/10.1115/1.4010089
Published Online: April 5, 2021
View Article titled, Some Experiments on the Interaction of Shock Waves With Boundary Layers on a Flat Plate
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Topics: Boundary layers, Flat plates, Shock waves, Shock (Mechanics), Boundary layer turbulence, Turbulence, Interferometers, Mach number, Reflection
Journal Articles

A Study of the Supersonic Axial-Flow Compressor

W. A. Loeb
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. March 1949, 16(1): 19–26.
https://doi.org/10.1115/1.4009890
Published Online: April 5, 2021
View Article titled, A Study of the Supersonic Axial-Flow Compressor
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Topics: Axial flow, Compressors, Shock (Mechanics), Rotors, Stators, Design, Flow (Dynamics), Mach number, Pressure
Journal Articles

Supersonic Diffusers for Wind Tunnels

E. P. Neumann, F. Lustwerk
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. June 1949, 16(2): 195–202.
https://doi.org/10.1115/1.4009935
Published Online: April 5, 2021
View Article titled, Supersonic Diffusers for Wind Tunnels
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Topics: Diffusers, Wind tunnels, Shock (Mechanics), Mach number, Boundary layers, Design, Geometry, Pressure, Separation (Technology)
Journal Articles

Tables for Numerical Solution of Problems in Compressible Gas Flow With Energy Effects

Ascher H. Shapiro, Gilbert M. Edelman
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Design Data And Methods
J. Appl. Mech. June 1948, 15(2): 169–175.
https://doi.org/10.1115/1.4009800
Published Online: March 12, 2021
View Article titled, Tables for Numerical Solution of Problems in Compressible Gas Flow With Energy Effects
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Topics: Gas flow, Combustion, Condensation, Explosions, Flames, Heat transfer, Mach number, Shock (Mechanics), Specific heat, Temperature
Journal Articles

Measurements of Friction in a Pipe for Subsonic and Supersonic Flow of Air

J. H. Keenan, E. P. Neumann
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. June 1946, 13(2): A91–A100.
https://doi.org/10.1115/1.4009532
Published Online: March 10, 2021
View Article titled, Measurements of Friction in a Pipe for Subsonic and Supersonic Flow of Air
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Topics: Friction, Pipes, Supersonic flow, Mach number, Reynolds number, Shock (Mechanics), Flow (Dynamics), Nozzles, Boundary layers, Compressible flow
Journal Articles

Effect of Variable Viscosity on Boundary Layers, With a Discussion of Drag Measurements

J. G. Brainerd, H. W. Emmons
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. March 1942, 9(1): A1–A6.
https://doi.org/10.1115/1.4009153
Published Online: March 3, 2021
View Article titled, Effect of Variable Viscosity on Boundary Layers, With a Discussion of Drag Measurements
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Topics: Boundary layers, Drag (Fluid dynamics), Viscosity, Temperature, Flow (Dynamics), Mach number, Equilibrium (Physics), Errors, Laminar flow, Nozzles
Journal Articles

Investigation of the Magnus Effect of a Generic Projectile at Mach 3 Up to 16 Degrees Angle of Attack

D. Klatt, R. Hruschka, F. Leopold
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Exterior Ballistics
J. Appl. Mech. May 2013, 80(3): 031603.
Paper No: JAM-12-1359
https://doi.org/10.1115/1.4023434
Published Online: April 19, 2013
View Article titled, Investigation of the Magnus Effect of a Generic Projectile at Mach 3 Up to 16 Degrees Angle of Attack
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Topics: Flow (Dynamics), Magnus effect, Pressure, Projectiles, Rotation, Spin (Aerodynamics), Wind tunnels, Vortices, Mach number, Flow visualization
Journal Articles

Improved One-Dimensional Unsteady Modeling of Thermally Choked Ram Accelerator in Subdetonative Velocity Regime

Tarek Bengherbia, Yufeng Yao, Pascal Bauer, Marc Giraud, Carl Knowlen
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. September 2011, 78(5): 051004.
https://doi.org/10.1115/1.4004327
Published Online: July 27, 2011
View Article titled, Improved One-Dimensional Unsteady Modeling of Thermally Choked Ram Accelerator in Subdetonative Velocity Regime
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Topics: Combustion, Computational fluid dynamics, Flow (Dynamics), Mach number, Modeling, Pressure, Projectiles, Thrust, Turbulence, Propulsion
Journal Articles

An Experimental Study on the Influence of Vortex Generators on the Shock-Induced Boundary Layer Separation at M = 1.4

A. Zare Shahneh, F. Motallebi
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. July 2009, 76(4): 041009.
https://doi.org/10.1115/1.3086591
Published Online: April 23, 2009
View Article titled, An Experimental Study on the Influence of Vortex Generators on the Shock-Induced Boundary Layer Separation at M = 1.4
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Topics: Boundary layers, Flow (Dynamics), Flow visualization, Generators, Pressure, Separation (Technology), Shock (Mechanics), Shock waves, Vortices, Shapes
Journal Articles

Design and Manufacture of a Morphing Structure for a Shape-Adaptive Supersonic Wind Tunnel Nozzle

Craig A. Steeves, Katherine H. Timpano, Peter T. Maxwell, Luigi Martinelli, Richard B. Miles
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Research Papers
J. Appl. Mech. May 2009, 76(3): 031012.
https://doi.org/10.1115/1.3005572
Published Online: March 11, 2009
View Article titled, Design and Manufacture of a Morphing Structure for a Shape-Adaptive Supersonic Wind Tunnel Nozzle
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Topics: Nozzles, Shapes, Wind tunnels, Design, Mach number, Shock (Mechanics), Flow (Dynamics)
Journal Articles

Computation of Inviscid Supersonic Flows Around Cylinders and Spheres With the V-SGS Stabilization and Y Z β Shock-Capturing

Franco Rispoli, Rafael Saavedra, Filippo Menichini, Tayfun E. Tezduyar
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Stabilized, Multiscale, And Multiphysics Methods In Fluid Mechanics
J. Appl. Mech. March 2009, 76(2): 021209.
https://doi.org/10.1115/1.3057496
Published Online: January 26, 2009
View Article titled, Computation of Inviscid Supersonic Flows Around Cylinders and Spheres With the V-SGS Stabilization and Y Z β Shock-Capturing
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Topics: Compressible flow, Computation, Cylinders, Flow (Dynamics), Mach number, Shock (Mechanics), Supersonic flow
Journal Articles

Large-Eddy Simulation of Reacting Turbulent Flows in Complex Geometries

K. Mahesh, G. Constantinescu, S. Apte, G. Iaccarino, F. Ham, P. Moin
Journal: Journal of Applied Mechanics
Publisher: ASME
Article Type: Technical Papers
J. Appl. Mech. May 2006, 73(3): 374–381.
https://doi.org/10.1115/1.2179098
Published Online: November 9, 2005
View Article titled, Large-Eddy Simulation of Reacting Turbulent Flows in Complex Geometries
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Topics: Combustion chambers, Flow (Dynamics), Gas turbines, Geometry, Turbulence, Density, Large eddy simulation, Combustion, Mach number