An Empirically Derived Basis For Calculating The Area Rate And Distribution Of Water Drop Impingement On Airfoils PDF Download

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Report

Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 52
Release: 1955
Genre: Aeronautics
ISBN:

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Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages:
Release: 1955
Genre: Aeronautics
ISBN:

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


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
Author: John A. Axelson
Publisher:
Total Pages: 696
Release: 1954
Genre: Aerodynamics
ISBN:

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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.


Research Abstracts

Research Abstracts
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 568
Release: 1951
Genre: Aeronautics
ISBN:

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Fallout Control

Fallout Control
Author: C. E. Lapple
Publisher:
Total Pages: 204
Release: 1958
Genre: Leukemia, Radiation-induced
ISBN:

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Annual Report

Annual Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 534
Release: 1953
Genre: Aeronautics
ISBN:

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