Wind-tunnel Investigation of an STOL Aircraft Configuration Equipped with an External-flow Jet Flap 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 Wind-tunnel Investigation of an STOL Aircraft Configuration Equipped with an External-flow Jet Flap PDF full book. Access full book title Wind-tunnel Investigation of an STOL Aircraft Configuration Equipped with an External-flow Jet Flap by Lysle P. Parlett. Download full books in PDF and EPUB format.
Author: Lysle P. Parlett
Publisher:
ISBN:
Category : Jet transports
Languages : en
Pages : 90
Get Book Here
Book Description
Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with external flow jet flap.
Author: Lysle P. Parlett
Publisher:
ISBN:
Category : Jet transports
Languages : en
Pages : 90
Get Book Here
Book Description
Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with external flow jet flap.
Author: Lysle P. Parlett
Publisher:
ISBN:
Category :
Languages : en
Pages : 85
Get Book Here
Book Description
Author: Lysle P. Parlett
Publisher:
ISBN:
Category : Jet transports
Languages : en
Pages : 84
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 464
Get Book Here
Book Description
Author: Delma C. Freeman
Publisher:
ISBN:
Category : Flaps (Airplanes)
Languages : en
Pages : 132
Get Book Here
Book Description
Author: Lysle P. Parlett
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 90
Get Book Here
Book Description
Author: Joseph L. Johnson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Get Book Here
Book Description
A wind-tunnel investigation at low speeds has been made to determine the flight characteristics of a model of a sweptback-wing jet-transport airplane equipped with an external-flow jet-augmented slotted flap. The model was flown in the flap-retracted configuration over a lift-coefficient range from 0.6 to 0.9 and in the flap-extended configuration over a-lift-coefficient range up to about 12.5 for a range of angles of attack from -12 to about 13 degrees. For tests at the very high lift coefficients, a downwardly directed nose jet was used to supplement the trinrming power of the horizontal tail.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 978
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 202
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
Get Book Here
Book Description
