Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description
Development and Analysis of a STOL Supersonic Cruise Fighter Concept
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description
Low-Speed Wind-Tunnel Test of a Stol Supersonic-Cruise Fighter Concept
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722350284
Category :
Languages : en
Pages : 46
Book Description
A wind-tunnel investigation was conducted to examine the low-speed static stability and control characteristics of a 0.10 scale model of a STOL supersonic cruise fighter concept. The concept, referred to as a twin boom fighter, was designed as a STOL aircraft capable of efficient long range supersonic cruise. The configuration name is derived from the long twin booms extending aft of the engine to the twin vertical tails which support a high center horizontal tail. The propulsion system features a two dimensional thrust vectoring exhaust nozzle which is located so that the nozzle hinge line is near the aircraft center of gravity. This arrangement is intended to allow large thrust vector angles to be used to obtain significant values of powered lift, while minimizing pitching moment trim changes. Low speed stability and control information was obtained over an angle of attack range including the stall. A study of jet induced power effects was included. Coe, Paul L., Jr. and Riley, Donald R. Langley Research Center RTOP 505-61-71-07...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722350284
Category :
Languages : en
Pages : 46
Book Description
A wind-tunnel investigation was conducted to examine the low-speed static stability and control characteristics of a 0.10 scale model of a STOL supersonic cruise fighter concept. The concept, referred to as a twin boom fighter, was designed as a STOL aircraft capable of efficient long range supersonic cruise. The configuration name is derived from the long twin booms extending aft of the engine to the twin vertical tails which support a high center horizontal tail. The propulsion system features a two dimensional thrust vectoring exhaust nozzle which is located so that the nozzle hinge line is near the aircraft center of gravity. This arrangement is intended to allow large thrust vector angles to be used to obtain significant values of powered lift, while minimizing pitching moment trim changes. Low speed stability and control information was obtained over an angle of attack range including the stall. A study of jet induced power effects was included. Coe, Paul L., Jr. and Riley, Donald R. Langley Research Center RTOP 505-61-71-07...
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 968
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 968
Book Description
Low-speed Wind-tunnel Test of a STOL Supersonic-cruise Fighter Concept
Author: Paul L. Coe
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 48
Book Description
Low-speed Wind-tunnel Test of a STOL Supersonic-cruise Fighter Concept
Author: Paul L. Coe
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Arrow-wing Supersonic Cruise Aircraft Structural Design Concepts Evaluation. Volume 1: Sections 1 Through 6
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 452
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 452
Book Description
Study of Metallic Structural Design Concepts for an Arrow Wing Supersonic Cruise Configuration
Author: M. J. Turner
Publisher:
ISBN:
Category : Supersonic planes
Languages : en
Pages : 166
Book Description
Publisher:
ISBN:
Category : Supersonic planes
Languages : en
Pages : 166
Book Description
Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1984
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 416
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 416
Book Description
Supersonic Cruise Military Aircraft Research
Author: Marie H. Tuttle
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 28
Book Description
Low-speed Wind-tunnel Test of a STOL Supersonic-cruise Fighter Concept
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description