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Investigation of Effect of Sideslip on Lateral Stability II: Rectangular Midwing on Circular Fuselage with Variations in Vertical Tail Area and Fuselage Length with and Without Horizontal Tail Surface (NACA Wartime Report L5C13)

Investigation of Effect of Sideslip on Lateral Stability II: Rectangular Midwing on Circular Fuselage with Variations in Vertical Tail Area and Fuselage Length with and Without Horizontal Tail Surface (NACA Wartime Report L5C13)

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Investigation of Effect of Sideslip on Lateral Stability II: Rectangular Midwing on Circular Fuselage with Variations in Vertical Tail Area and Fuselage Length with and Without Horizontal Tail Surface (NACA Wartime Report L5C13)

by Thomas A. Hollingworth

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  • Paperback
Condition
Good Condition
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About This Item

NACA/National Advisory Committee for Aeronautics, 1945. Softcover. Good Condition. Illustrator: . A couple library stamps and pencil notes on covers. Stapled edge, light wear, yellowing to the covers and pages but a good solid booklet overall. Illustrator: . Quantity Available: 1. Category: Aviation; Inventory No: 153401. .

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Details

Bookseller
Easy Chair Books US (US)
Bookseller's Inventory #
153401
Title
Investigation of Effect of Sideslip on Lateral Stability II: Rectangular Midwing on Circular Fuselage with Variations in Vertical Tail Area and Fuselage Length with and Without Horizontal Tail Surface (NACA Wartime Report L5C13)
Author
Thomas A. Hollingworth
Illustrator
Format/Binding
Softcover
Book Condition
Used - Good Condition
Quantity Available
1
Binding
Paperback
Publisher
NACA/National Advisory Committee for Aeronautics
Date Published
1945
Keywords
BZDB23 Aviation; UPC: Original Thomas A. Hollingworth Investigation of Effect of Sideslip on Lateral Stability II: Rectangular Midwing on Circular Fuselage with Variations in Vertical Tail Area and Fuselage Length with and Without Horizontal Tail Surf
Bookseller catalogs
Aviation;

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About the Seller

Easy Chair Books

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This seller has earned a 5 of 5 Stars rating from Biblio customers.
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Lexington, Missouri

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