NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Aerodynamics of thrust vectoringThrust vectoring as a means to enhance maneuverability and aerodynamic performane of a tactical aircraft is discussed. This concept usually involves the installation of a multifunction nozzle. With the nozzle, the engine thrust can be changed in direction without changing the attitude of the aircraft. Change in the direction of thrust induces a significant change in the aerodynamic forces on the aircraft. Therefore, this device can be used for lift-augmenting as well as stability and control purposes. When the thrust is deflected in the longitudinal direction, the lift force and the pitching stability can be manipulated, while the yawing stability can be controlled by directing the thrust in the lateral direction.
Document ID
19900004038
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tseng, J. B. (Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Lan, C. Edward (Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:185074
NASA-CR-185074
Accession Number
90N13354
Funding Number(s)
CONTRACT_GRANT: NAG1-837
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available