Flying Aircraft Carriers of the USAF: Wing Tip Coupling

Flying Aircraft Carriers of the USAF: Wing Tip Coupling
Author: Brian Lockett
Publisher: Lulu.com
Total Pages: 102
Release: 2009-07-01
Genre: History
ISBN: 0578031868


Download Flying Aircraft Carriers of the USAF: Wing Tip Coupling Book in PDF, Epub and Kindle

During and after World War II, aircraft designers were faced with the problem of increasing the range of strategic bombers. Dr. Richard Vogt, a German immigrant to the United States, proposed that floating wing panels carrying fuel tanks could be attached to the wing tips of an airplane with hinges to extend its range. The floating wing panels would support their own weight, without increasing the load on the airplane's wings. The Air Force initiated a project to simulate floating wing panels with a piloted light plane that coupled to a larger airplane in flight. Soon the scope of the project expanded to explore the possibility of towing fighters coupled to the wing tips of bombers.


Flying Aircraft Carriers of the USAF: Wing Tip Coupling
Language: en
Pages: 102
Authors: Brian Lockett
Categories: History
Type: BOOK - Published: 2009-07-01 - Publisher: Lulu.com

GET EBOOK

During and after World War II, aircraft designers were faced with the problem of increasing the range of strategic bombers. Dr. Richard Vogt, a German immigrant
Wing Engineering: Aerodynamics, Structures And Design
Language: en
Pages: 208
Authors: Samuel Merryisha, Parvathy Rajendran
Categories: Technology & Engineering
Type: BOOK - Published: 2023-10-11 - Publisher: Penerbit USM

GET EBOOK

The advancement of flight science and technology has shown much boom contribution towards the aircraft wing and its retrofitting. Looking into the aircraft wing
Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9
Language: en
Pages: 28
Authors: Harold Mirels
Categories: Aerodynamic load
Type: BOOK - Published: 1949 - Publisher:

GET EBOOK

An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution over a wing tip in a region influenced by a sharp subsonic t
Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5
Language: en
Pages: 180
Authors: Victor L. Peterson
Categories: Aerodynamics
Type: BOOK - Published: 1960 - Publisher:

GET EBOOK

Comparison of Tail and Wing-tip Spin-recovery Parachutes as Determined by Tests in the Langley 20-foot Free-spinning Tunnel
Language: en
Pages: 66
Authors: Robert William Kamm
Categories: Aerodynamics
Type: BOOK - Published: 1946 - Publisher:

GET EBOOK

Summary: Tests of spin-recovery parachutes on six models of typical fighter and trainer airplanes were conducted in the Langley 20-foot free-spinning tunnel to