Effect of Elevator-profile Modifications and Trailing-edge Strips on Elevator Hinge-moment and Other Aerodynamic Characteristics of a Full-scale Horizontal Tail Surface PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Effect of Elevator-profile Modifications and Trailing-edge Strips on Elevator Hinge-moment and Other Aerodynamic Characteristics of a Full-scale Horizontal Tail Surface PDF full book. Access full book title Effect of Elevator-profile Modifications and Trailing-edge Strips on Elevator Hinge-moment and Other Aerodynamic Characteristics of a Full-scale Horizontal Tail Surface by Carl F. Schueller. Download full books in PDF and EPUB format.
Author: Carl F. Schueller
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 64
Get Book Here
Book Description
Summary: Results are presented of tests of a full-scale horizontal tail surface made to determine the effect of elevator-profile modifications and trailing-edge strips on the elevator hinge-moment characteristics for elevators having fixed plan form and constant balance.
Author: Carl F. Schueller
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 64
Get Book Here
Book Description
Summary: Results are presented of tests of a full-scale horizontal tail surface made to determine the effect of elevator-profile modifications and trailing-edge strips on the elevator hinge-moment characteristics for elevators having fixed plan form and constant balance.
Author: Langley Aeronautical Laboratory
Publisher: Hassell Street Press
ISBN: 9781014247902
Category :
Languages : en
Pages : 64
Get Book Here
Book Description
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 86
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 188
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Get Book Here
Book Description
Author: William K. Ritter
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 560
Get Book Here
Book Description
It was concluded that the volume flow capacity of a conventional-type radial-discharge impeller may be greatly increased by utilizing a rear shroud profile of large radius of curvature and a large impeller axial depth to give a gradual change in direction tthrough the impeller passage.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 426
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 916
Get Book Here
Book Description
