NDLI: Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface f-15 model at transonic speeds

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Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface f-15 model at transonic speeds

Content Provider	NASA Technical Reports Server (NTRS)
Author	Bare, E. A. Pendergraft Jr., O. C.
Copyright Year	1983
Description	An investigation was conducted in the Langley 16 Foot Transonic Tunnel to determine the lateral directional aerodynamic characteristics of a fully metric 0.04 scale model of the F-15 three surface configuration (canards, horizontal tails) with twin two dimensional nozzles and twin axisymmetric nozzles installed. The effects of two dimensional nozzle in flight thrust reversing and rudder deflection were also determined. Test data were obtained at static conditions and at Mach numbers from 0.60 to 1.20 over an angle of attack range from -2 deg to 15 deg. Reynolds number varied from 2.6 million to 3.8 million. Angle of sideslip was set at approximately 0 deg and -5 deg for all configurations and at -10 deg for selected configurations.
File Size	4672903
Page Count	92
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19840005097
Archival Resource Key	ark:/13960/t5p894044
Language	English
Publisher Date	1983-12-01
Access Restriction	Open
Subject Keyword	Aerodynamics Tail Assemblies Nozzle Design Wings Canard Configurations Rudders Transonic Wind Tunnels Thrust Reversal Aerodynamic Coefficients Wind Tunnel Models F-15 Aircraft Propulsion System Configurations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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