The Effect of Variations in Moments of Inertia on Spin and Recovery Characteristics of a Single-engine Low-wing Monoplane with Various Tail Arrangements Including a Twin Tail PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download The Effect of Variations in Moments of Inertia on Spin and Recovery Characteristics of a Single-engine Low-wing Monoplane with Various Tail Arrangements Including a Twin Tail PDF full book. Access full book title The Effect of Variations in Moments of Inertia on Spin and Recovery Characteristics of a Single-engine Low-wing Monoplane with Various Tail Arrangements Including a Twin Tail by Anshal I. Neihouse. Download full books in PDF and EPUB format.
Author: Anshal I. Neihouse
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 50
Get Book Here
Book Description
Results of an investigation made in the Langley 15-foot free-spinning tunnel of the effects of variation of the moment of inertia of a research model representative of a present-day trainer or a four-place cabin monoplane are presented. Eight different wing arrangements and four different tail arrangements, including a twin tail, were tested. The moments of inertia about the three airplane axes were increased or decreased by a constant percentage and the results were compared. These results were also compared with results previously presented for variation of the airplane relative density.
Author: Anshal I. Neihouse
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 50
Get Book Here
Book Description
Results of an investigation made in the Langley 15-foot free-spinning tunnel of the effects of variation of the moment of inertia of a research model representative of a present-day trainer or a four-place cabin monoplane are presented. Eight different wing arrangements and four different tail arrangements, including a twin tail, were tested. The moments of inertia about the three airplane axes were increased or decreased by a constant percentage and the results were compared. These results were also compared with results previously presented for variation of the airplane relative density.
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 690
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 446
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 666
Get Book Here
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Get Book Here
Book Description
Author: David R. Ellis
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 116
Get Book Here
Book Description
Although the stall/spin accident record has improved significantly since the 1945-1948 period, the stall-related accident still accounts for a large percentage of general aviation fatalities. This study represents an effort to obtain a better understanding of the circumstances, causes, and factors which result in unintentional stalls at low altitude. A three-part program was conducted, involving extensive computer analysis of stall-related accidents for the period 1965-1973, flight evaluation of the low speed handling qualities and stall behavior of seven lightplanes, and generalized experiments to study pilot/airplane interactions in the high angle of attack regime using an in-flight simulator. The results indicate that further work is especially warranted in the areas of pilot education and training, stall warning systems, and application of new aerodynamic technology. In addition, renewed consideration should be given to the idea of limiting control power in non-acrobatic airplanes. (Author).
Author: United States. Federal Aviation Administration. Systems Research and Development Service
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 622
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
Get Book Here
Book Description
