AIAA 71-1 - AIAA 71-40

AIAA 71-1 - AIAA 71-40 PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 592

Get Book Here

Book Description


AIAA 71-106 - AIAA 71-155

AIAA 71-106 - AIAA 71-155 PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702

Get Book Here

Book Description


AIAA 71-156 - AIAA 71-217. (With omissions in numbering)

AIAA 71-156 - AIAA 71-217. (With omissions in numbering) PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :

Get Book Here

Book Description


AIAA 71-66 - AIAA 71-105

AIAA 71-66 - AIAA 71-105 PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 496

Get Book Here

Book Description


AIAA 71-681 - AIAA 71-725

AIAA 71-681 - AIAA 71-725 PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :

Get Book Here

Book Description


AIAA 71-728 - AIAA 71-760. (With omissions in numbering)

AIAA 71-728 - AIAA 71-760. (With omissions in numbering) PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :

Get Book Here

Book Description


AIAA 71-41 - AIAA 71-65

AIAA 71-41 - AIAA 71-65 PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 466

Get Book Here

Book Description


Ground and Flight Evaluation of a Small-Scale Inflatable-Winged Aircraft

Ground and Flight Evaluation of a Small-Scale Inflatable-Winged Aircraft PDF Author:
Publisher:
ISBN:
Category : Air-supported structures
Languages : en
Pages : 24

Get Book Here

Book Description
A small-scale, instrumented research aircraft was flown to investigate the flight characteristics of inflatable wings. Ground tests measured the static structural characteristics of the wing at different inflation pressures, and these results compared favorably with analytical predictions. A research-quality instrumentation system was assembled, largely from commercial off-the-shelf components, and installed in the aircraft. Initial flight operations were conducted with a conventional rigid wing having the same dimensions as the inflatable wing. Subsequent flights were conducted with the inflatable wing. Research maneuvers were executed to identify the trim, aerodynamic performance, and longitudinal stability and control characteristics of the vehicle in its different wing configurations. For the angle-of-attack range spanned in this flight program.

AIAA 71-631 - AIAA 71-680

AIAA 71-631 - AIAA 71-680 PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :

Get Book Here

Book Description


Fundamentals of Aircraft and Airship Design

Fundamentals of Aircraft and Airship Design PDF Author: Leland Malcolm Nicolai
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 940

Get Book Here

Book Description
The aircraft is only a transport mechanism for the payload, and all design decisions must consider payload first. Simply stated, the aircraft is a dust cover. "Fundamentals of Aircraft and Airship Design, Volume 1: Aircraft Design" emphasizes that the science and art of the aircraft design process is a compromise and that there is no right answer; however, there is always a best answer based on existing requirements and available technologies.