Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 592
Book Description
AIAA 71-1 - AIAA 71-40
AIAA 71-106 - AIAA 71-155
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
AIAA 71-156 - AIAA 71-217. (With omissions in numbering)
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
Book Description
AIAA 71-66 - AIAA 71-105
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 496
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 496
Book Description
AIAA 71-681 - AIAA 71-725
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :
Book Description
AIAA 71-728 - AIAA 71-760. (With omissions in numbering)
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :
Book Description
AIAA 71-41 - AIAA 71-65
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 466
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 466
Book Description
Ground and Flight Evaluation of a Small-Scale Inflatable-Winged Aircraft
Author:
Publisher:
ISBN:
Category : Air-supported structures
Languages : en
Pages : 24
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.
Publisher:
ISBN:
Category : Air-supported structures
Languages : en
Pages : 24
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
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :
Book Description
Fundamentals of Aircraft and Airship Design
Author: Leland Malcolm Nicolai
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 940
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.
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 940
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.