Author: Linda S. Bangert
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 272
Book Description
Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers
Author: Linda S. Bangert
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 272
Book Description
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 272
Book Description
Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723563997
Category :
Languages : en
Pages : 272
Book Description
A parametric study was conducted in the Langley 16-Foot Transonic Tunnel on an isolated nonaxisymmetic fuselage model that simulates a twin-engine fighter. The effects of aft-end closure distribution (top/bottom) nozzle-flap boattail angle versus nozzle-sidewall boattail angle) and afterbody and nozzle corner treatment (sharp or radius) were investigated. Four different closure distributions with three different corner radii were tested. Tests were conducted over a range of Mach numbers from 0.40 to 1.25 and over a range of angles of attack from -3 to 9 degrees. Solid plume simulators were used to simulate the jet exhaust. For a given closure distribution in the range of Mach numbers tested, the sharp-corner nozzles generally had the highest drag, and the 2-in. corner-radius nozzles generally had the lowest drag. The effect of closure distribution on afterbody drag was highly dependent on configuration and flight condition. Bangert, Linda S. and Carson, George T., Jr. Langley Research Center NASA-TP-3236, L-17034, NAS 1.60:3236 RTOP 505-62-30-01...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723563997
Category :
Languages : en
Pages : 272
Book Description
A parametric study was conducted in the Langley 16-Foot Transonic Tunnel on an isolated nonaxisymmetic fuselage model that simulates a twin-engine fighter. The effects of aft-end closure distribution (top/bottom) nozzle-flap boattail angle versus nozzle-sidewall boattail angle) and afterbody and nozzle corner treatment (sharp or radius) were investigated. Four different closure distributions with three different corner radii were tested. Tests were conducted over a range of Mach numbers from 0.40 to 1.25 and over a range of angles of attack from -3 to 9 degrees. Solid plume simulators were used to simulate the jet exhaust. For a given closure distribution in the range of Mach numbers tested, the sharp-corner nozzles generally had the highest drag, and the 2-in. corner-radius nozzles generally had the lowest drag. The effect of closure distribution on afterbody drag was highly dependent on configuration and flight condition. Bangert, Linda S. and Carson, George T., Jr. Langley Research Center NASA-TP-3236, L-17034, NAS 1.60:3236 RTOP 505-62-30-01...
First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop
Author: Richard M. Wood
Publisher:
ISBN:
Category : High-speed aeronautics
Languages : en
Pages : 354
Book Description
Publisher:
ISBN:
Category : High-speed aeronautics
Languages : en
Pages : 354
Book Description
Scientific and Technical Aerospace Reports
NASA Scientific and Technical Publications
NASA Scientific and Technical Publications: A Catalog of Special Publications, Reference Publications, Conference Publications, and Technical Papers, 1991-1992
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 720
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 720
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1786
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1786
Book Description
The NASA Langley 16-foot Transonic Tunnel: Historical Overview, Facility Description, Calibration, Flow Characteristics, and Test Capabilities
Author: Francis J. Capone
Publisher:
ISBN:
Category : Transonic wind tunnels
Languages : en
Pages : 208
Book Description
Publisher:
ISBN:
Category : Transonic wind tunnels
Languages : en
Pages : 208
Book Description