Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds

Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds
Author :
Publisher :
Total Pages : 692
Release :
ISBN-10 : STANFORD:36105024832094
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds by : James W. Wiggins

Download or read book Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds written by James W. Wiggins and published by . This book was released on 1956 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the horizontal- and vertical-tail contributions to the static lateral stability of a complete-model swept-wing configuration at high subsonic speeds. The results indicate that, in a general, Mach number effects within the range studied and wing effects on the tail contribution were small and the overall trends of the data of the present investigation agreed with those which have been established at low speeds.


Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds Related Books

Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds
Language: en
Pages: 692
Authors: James W. Wiggins
Categories: Airplanes
Type: BOOK - Published: 1956 - Publisher:

DOWNLOAD EBOOK

An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the horizontal- and vertical-tail contributions to the static lateral
Technical Note - National Advisory Committee for Aeronautics
Language: en
Pages: 1026
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1956 - Publisher:

DOWNLOAD EBOOK

Technical Note
Language: en
Pages: 510
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1956 - Publisher:

DOWNLOAD EBOOK

Research Abstracts and Reclassification Notice
Language: en
Pages: 508
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1954 - Publisher:

DOWNLOAD EBOOK

Report
Language: en
Pages: 620
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1945 - Publisher:

DOWNLOAD EBOOK