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BOOKS

Books

12 total

Too Many Bunnies (Neal Porter Books)

Matt Novak

2005PDF7.9 MB

To Mary Neal Kirkland and Our Many Friends in Andia

PDF20 MB

Boundary-layer Measurements in Accelerated Flows Near Mach 1

Howard L. Wesoky

1967

Boundary-layer Transition on Cones Near Mach One in an Aeroballistic Range

J. Leith Potter

1975

Computation of the Potential Function of a Compressible Fluid Near Mach Number 1

Howard. Tashjian

1970

An Exploratory Investigation of a Transport Configuration Designed for Supersonic Cruise Flight Near a Mach Number of 3

Ausley B. Carraway

1960

The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0

W. F. Lindsey

1954

STUDY GUIDES & COMPANIONS

Study guides & companions

1 total

Analysis of Sonic Boom Measurements Near Shock Wave Extremities for Flight Near Mach 1.0 and for Airplane Accelerations

George T. Haglund

Study guidezipen1974

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DOCUMENTS · SCRIBD

Documents

1 total

Macy

Saurabhkumar Singh

Read now

All matching files

Other editions and formats

Individual editions and file formats that weren't grouped into the works above. Use this when you need a specific format, language, or scan quality.

5 of 13

Highly Sensitive Temperature Sensor Based on Cascaded Polymer-Infiltrated Fiber Mach–Zehnder Interferometers Operating near the Dispersion Turning Point

Jia He, Fengchan Zhang & 7 more

PDF6.3 MB

Experimental Studies of the Unstedy Aerodynamics of Panels at or Near Flutter with a Finite Boundary Layer Mach Number 1 to 10 / G. W. Asher and A. W. Brown.

G. Asher

1964

Surface Flow and Heating Distributions on a Cylinder in Near Wake of Aeroassist Flight Experiment (AFE) Configuration at Incidence in Mach 10 Air

William L. Wells

1990

Near-field Sonic-boom Pressure Signatures for the Space Shuttle Launch and Orbiter Vehicles at Mach 6 / George C. Ashby, Jr. Langley Research Center.

George C. Ashby

1979

Heat-transfer and pressure measurements on a simulated elevon deflected 30 ̊near flight conditions at Mach 7 / Charles B. Johnson, Allan H. Taylor, and Irving Weinstein.

Charles B. Johnson

1977

Genres

Books

Too Many Bunnies (Neal Porter Books)

To Mary Neal Kirkland and Our Many Friends in Andia

Boundary-layer Measurements in Accelerated Flows Near Mach 1

Boundary-layer Transition on Cones Near Mach One in an Aeroballistic Range

Computation of the Potential Function of a Compressible Fluid Near Mach Number 1

An Exploratory Investigation of a Transport Configuration Designed for Supersonic Cruise Flight Near a Mach Number of 3

The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0

Study guides & companions

Analysis of Sonic Boom Measurements Near Shock Wave Extremities for Flight Near Mach 1.0 and for Airplane Accelerations

Documents

Macy

Other editions and formats

Highly Sensitive Temperature Sensor Based on Cascaded Polymer-Infiltrated Fiber Mach–Zehnder Interferometers Operating near the Dispersion Turning Point

Experimental Studies of the Unstedy Aerodynamics of Panels at or Near Flutter with a Finite Boundary Layer Mach Number 1 to 10 / G. W. Asher and A. W. Brown.

Surface Flow and Heating Distributions on a Cylinder in Near Wake of Aeroassist Flight Experiment (AFE) Configuration at Incidence in Mach 10 Air

Near-field Sonic-boom Pressure Signatures for the Space Shuttle Launch and Orbiter Vehicles at Mach 6 / George C. Ashby, Jr. Langley Research Center.

Heat-transfer and pressure measurements on a simulated elevon deflected 30 ̊near flight conditions at Mach 7 / Charles B. Johnson, Allan H. Taylor, and Irving Weinstein.

Genres

Genres

Books

Too Many Bunnies (Neal Porter Books)

To Mary Neal Kirkland and Our Many Friends in Andia

Boundary-layer Measurements in Accelerated Flows Near Mach 1

Boundary-layer Transition on Cones Near Mach One in an Aeroballistic Range

Computation of the Potential Function of a Compressible Fluid Near Mach Number 1

An Exploratory Investigation of a Transport Configuration Designed for Supersonic Cruise Flight Near a Mach Number of 3

The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0

Study guides & companions

Analysis of Sonic Boom Measurements Near Shock Wave Extremities for Flight Near Mach 1.0 and for Airplane Accelerations

Documents

Macy

Other editions and formats

Highly Sensitive Temperature Sensor Based on Cascaded Polymer-Infiltrated Fiber Mach–Zehnder Interferometers Operating near the Dispersion Turning Point

Experimental Studies of the Unstedy Aerodynamics of Panels at or Near Flutter with a Finite Boundary Layer Mach Number 1 to 10 / G. W. Asher and A. W. Brown.

Surface Flow and Heating Distributions on a Cylinder in Near Wake of Aeroassist Flight Experiment (AFE) Configuration at Incidence in Mach 10 Air

Near-field Sonic-boom Pressure Signatures for the Space Shuttle Launch and Orbiter Vehicles at Mach 6 / George C. Ashby, Jr. Langley Research Center.

Heat-transfer and pressure measurements on a simulated elevon deflected 30 ̊near flight conditions at Mach 7 / Charles B. Johnson, Allan H. Taylor, and Irving Weinstein.