An Empirically Derived Basis for Calculating the Area, Rate, and Distribution of Water-drop Impingement on Airfoils

An Empirically Derived Basis for Calculating the Area, Rate, and Distribution of Water-drop Impingement on Airfoils
Author :
Publisher :
Total Pages : 346
Release :
ISBN-10 : OSU:32435065611972
ISBN-13 :
Rating : 4/5 (72 Downloads)

Book Synopsis An Empirically Derived Basis for Calculating the Area, Rate, and Distribution of Water-drop Impingement on Airfoils by : Antonio Ferri

Download or read book An Empirically Derived Basis for Calculating the Area, Rate, and Distribution of Water-drop Impingement on Airfoils written by Antonio Ferri and published by . This book was released on 1952 with total page 346 pages. Available in PDF, EPUB and Kindle. Book excerpt:


An Empirically Derived Basis for Calculating the Area, Rate, and Distribution of Water-drop Impingement on Airfoils Related Books

An Empirically Derived Basis for Calculating the Area, Rate, and Distribution of Water-drop Impingement on Airfoils
Language: en
Pages: 346
Authors: Antonio Ferri
Categories: Aerodynamic load
Type: BOOK - Published: 1952 - Publisher:

DOWNLOAD EBOOK

Report
Language: en
Pages: 52
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1955 - Publisher:

DOWNLOAD EBOOK

Annual Report - National Advisory Committee for Aeronautics
Language: en
Pages:
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1955 - Publisher:

DOWNLOAD EBOOK

Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Report - National Advisory Committee for Aeronautics
Language: en
Pages: 1208
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1952 - Publisher:

DOWNLOAD EBOOK

Investigation of a Slat in Several Different Positions on an NACA 64A010 Airfoil for a Wide Range of Subsonic Mach Numbers
Language: en
Pages: 696
Authors: John A. Axelson
Categories: Aerodynamics
Type: BOOK - Published: 1954 - Publisher:

DOWNLOAD EBOOK

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