Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers PDF Download

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Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers

Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers PDF Author: Richard D. Samuels
Publisher:
ISBN:
Category : Skim friction (Aerodynamics)
Languages : en
Pages : 82

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Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers

Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers PDF Author: Richard D. Samuels
Publisher:
ISBN:
Category : Skim friction (Aerodynamics)
Languages : en
Pages : 82

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Book Description

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 496

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Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers

Experimental Investigation of a Hypersonic Glider Configuration at a Mach Number of 6 and at Full-scale Reynolds Numbers PDF Author: Alvin Seiff
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 74

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1146

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Noise Survey of a Full-scale Supersonic Turbine-driven Propeller Under Static Conditions

Noise Survey of a Full-scale Supersonic Turbine-driven Propeller Under Static Conditions PDF Author: Max C. Kurbjun
Publisher:
ISBN:
Category : Noise
Languages : en
Pages : 742

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Overall sound-pressure levels and frequency spectra of the noise emitted from a full-scale, 7.2-foot-diameter, 3, 500 rpm, three-blade, supersonic propeller mounted on a turbine-powered airplane have been obtained under static conditions at stations about the propeller at a 100-foot radius.

Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508

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Book Description

A New Dimension, Wallops Island Flight Test Range

A New Dimension, Wallops Island Flight Test Range PDF Author: Joseph Adams Shortal
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 796

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WADC Technical Note

WADC Technical Note PDF Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category :
Languages : en
Pages : 1576

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A Review of Measurements on AGARD Calibration Models

A Review of Measurements on AGARD Calibration Models PDF Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher:
ISBN:
Category : Measurement
Languages : en
Pages : 272

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Systems Preliminary Design

Systems Preliminary Design PDF Author: Joseph J. Jerger
Publisher:
ISBN:
Category : Automatic control
Languages : en
Pages : 648

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Book Description