Method for Calculating Lift Distributions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data

Method for Calculating Lift Distributions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data
Author :
Publisher :
Total Pages : 70
Release :
ISBN-10 : UOM:39015086495044
ISBN-13 :
Rating : 4/5 (44 Downloads)

Book Synopsis Method for Calculating Lift Distributions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data by : James C. Sivells

Download or read book Method for Calculating Lift Distributions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data written by James C. Sivells and published by . This book was released on 1951 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for calculating lift distributions for unswept wings with flaps or ailerons using nonlinear section lift data. This method is based upon lifting-line theory and is an extension to the method described by NACA Report 865. Simplified computing forms containing detailed examples are given for both symmetrical and asymmetrical lift distributions. A few comparisons of experimental and calculated characteristics are also presented.


Method for Calculating Lift Distributions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data Related Books

Method for Calculating Lift Distributions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data
Language: en
Pages: 70
Authors: James C. Sivells
Categories: Aeronautics
Type: BOOK - Published: 1951 - Publisher:

DOWNLOAD EBOOK

A method is presented for calculating lift distributions for unswept wings with flaps or ailerons using nonlinear section lift data. This method is based upon l
Method for Calculating Lift Distribtutions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data
Language: en
Pages: 722
Authors: James C. Sivells
Categories: Ailerons
Type: BOOK - Published: 1951 - Publisher:

DOWNLOAD EBOOK

A method is presented for calculating lift distributions for unswept wings with flaps or ailerons using nonlinear section lift data. This method is based upon l
Annual Report of the National Advisory Committee for Aeronautics
Language: en
Pages: 1200
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1954 - 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: 1462
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1951 - Publisher:

DOWNLOAD EBOOK

Report
Language: en
Pages: 32
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1954 - Publisher:

DOWNLOAD EBOOK