Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 770
Book Description
NASA Technical Note
Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution
Author: Raul J. Conti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution
Author: Raul Jorge Conti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
NASA Memorandum
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 644
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 644
Book Description
NASA Memorandum
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1146
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1146
Book Description
Heat Transfer in the Turbulent Incompressible Boundary Layer with Constant and Variable Wall Temperature
Author: William C. Reynolds
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 500
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 500
Book Description
Noise Survey of a Full-scale Supersonic Turbine-driven Propeller Under Static Conditions
Author: Max C. Kurbjun
Publisher:
ISBN:
Category : Noise
Languages : en
Pages : 742
Book Description
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.
Publisher:
ISBN:
Category : Noise
Languages : en
Pages : 742
Book Description
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.
NASA Republication
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 146
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 146
Book Description
NASA Memorandum
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 590
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 590
Book Description