Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections

Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections
Author :
Publisher :
Total Pages : 20
Release :
ISBN-10 : OCLC:1109592231
ISBN-13 :
Rating : 4/5 (31 Downloads)

Book Synopsis Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections by : Homer B. Jr Wilson

Download or read book Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections written by Homer B. Jr Wilson and published by . This book was released on 1952 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections Related Books

Investigation at a Mach Number of 1.2 of Two 45 Degree Sweptback Wings Utilizing NACA 2-006 and NACA 65A006 Airfoil Sections
Language: en
Pages: 20
Wind-tunnel Investigation at High and Low Subsonic Mach Numbers of Two Unswept Wings Having NACA 2-006 and NACA 65A006 Airfoil Sections
Language: en
Pages: 40
USAF Stability and Control Datcom
Language: en
Pages: 642
Authors: Douglas Aircraft Company
Categories: Airplanes
Type: BOOK - Published: 1975 - Publisher:

DOWNLOAD EBOOK