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An Analytical Study of Heat Requirements for Icing Protection of Radomes

An Analytical Study of Heat Requirements for Icing Protection of Radomes PDF Author: James P. Lewis
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 24

Book Description

An Analytical Study of Heat Requirements for Icing Protection of Radomes

An Analytical Study of Heat Requirements for Icing Protection of Radomes PDF Author: James P. Lewis
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 24

Book Description

NACA Research Memorandum

NACA Research Memorandum PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 50

Book Description

Research Memorandum

Research Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 26

Book Description

Aircraft Ice Protection

Aircraft Ice Protection PDF Author: United States. Federal Aviation Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 60

Book Description

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 : 994

Book Description

Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category :
Languages : en
Pages : 596

Book Description

Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620

Book Description

Investigation of a Slat in Several Different Positions on an NACA 64A010 Airfoil for a Wide Range of Subsonic Mach Numbers

Investigation of a Slat in Several Different Positions on an NACA 64A010 Airfoil for a Wide Range of Subsonic Mach Numbers PDF Author: John A. Axelson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 696

Book Description
An investigation of the two-dimensional aerodynamic characteristics of an NACA 64A010 airfoil with a slat has been conducted in the Mach number range from 0.25 to 0.85, with a corresponding Reynolds number range from 3.4 million to 8.1 million. Two families of slat positions were investigated, one with the slat leading edge extended forward along the airfoil chord line, and the other with the slat extended forward and displaced below the chord line.

Annual Report

Annual Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 534

Book Description

Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :

Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
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