Author : David M. Schuster
Publisher : Unknown
Page : 44 pages
File Size : 54,5 Mb
Release : 2001
Category : Plates (Engineering)
ISBN : NASA:31769000642432
Aerodynamic Measurements On A Large Splitter Plate For The Nasa Langley Transonic Dynamics Tunnel
Aerodynamic Measurements On A Large Splitter Plate For The Nasa Langley Transonic Dynamics Tunnel Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Aerodynamic Measurements On A Large Splitter Plate For The Nasa Langley Transonic Dynamics Tunnel book. This book definitely worth reading, it is an incredibly well-written.
Aerodynamic Measurements on a Large Splitter Plate for the NASA Langley Transonic Dynamics Tunnel
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 42 pages
File Size : 47,5 Mb
Release : 2018-05-29
Category : Electronic
ISBN : 1720372969
Aerodynamic Measurements on a Large Splitter Plate for the NASA Langley Transonic Dynamics Tunnel by National Aeronautics and Space Administration (NASA) Pdf
Tests conducted in the NASA Langley Research Center Transonic Dynamics Tunnel (TDT) assess the aerodynamic characteristics of a splitter plate used to test some semispan models in this facility. Aerodynamic data are analyzed to determine the effect of the splitter plate on the operating characteristics of the TDT, as well as to define the range of conditions over which the plate can be reasonably used to obtain aerodynamic data. Static pressures measurements on the splitter plate surface and the equipment fairing between the wind tunnel wall and the splitter plate are evaluated to determine the flow quality around the apparatus over a range of operating conditions. Boundary layer rake data acquired near the plate surface define the viscous characteristics of the flow over the plate. Data were acquired over a range of subsonic, transonic and supersonic conditions at dynamic pressures typical for models tested on this apparatus. Data from this investigation should be used as a guide for the design of TDT models and tests using the splitter plate, as well as to guide future splitter plate design for this facility.Schuster, David M.Langley Research CenterTRANSONIC WIND TUNNELS; AERODYNAMIC CHARACTERISTICS; DYNAMIC PRESSURE; STATIC PRESSURE; VISCOUS FLOW; WIND TUNNEL TESTS; BOUNDARY LAYERS; SEMISPAN MODELS
Monthly Catalog of United States Government Publications
Author : Anonim
Publisher : Unknown
Page : 882 pages
File Size : 40,7 Mb
Release : 2003
Category : Government publications
ISBN : WISC:89085732485
Monthly Catalog of United States Government Publications by Anonim Pdf
NASA Langley Scientific and Technical Information Output-2001
Author : Anonim
Publisher : Unknown
Page : 166 pages
File Size : 55,5 Mb
Release : 2002
Category : Electronic
ISBN : NASA:31769000645625
NASA Langley Scientific and Technical Information Output-2001 by Anonim Pdf
Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Page : 704 pages
File Size : 47,6 Mb
Release : 1995
Category : Aeronautics
ISBN : UIUC:30112050127304
Scientific and Technical Aerospace Reports by Anonim Pdf
NASA Technical Memorandum
Author : Anonim
Publisher : Unknown
Page : 464 pages
File Size : 52,7 Mb
Release : 1990
Category : Aeronautics
ISBN : MINN:31951P00161764D
NASA Technical Memorandum by Anonim Pdf
NASA SP.
Author : Anonim
Publisher : Unknown
Page : 654 pages
File Size : 49,9 Mb
Release : 1992
Category : Aeronautics
ISBN : MINN:31951P00163367D
NASA SP. by Anonim Pdf
NASA Scientific and Technical Publications
Author : Anonim
Publisher : Unknown
Page : 410 pages
File Size : 51,7 Mb
Release : 1987
Category : Aeronautics
ISBN : STANFORD:36105024716149
NASA Scientific and Technical Publications by Anonim Pdf
Aeronautical Engineering
Author : Anonim
Publisher : Unknown
Page : 538 pages
File Size : 51,9 Mb
Release : 1991
Category : Aeronautics
ISBN : UOM:39015023295143
Aeronautical Engineering by Anonim Pdf
Optical Diagnostics for Fluids/heat/combustion and Photomechanics for Solids
Author : Soyoung S. Cha,P. Bryanston-Cross,Carolyn Regan Mercer
Publisher : SPIE-International Society for Optical Engineering
Page : 426 pages
File Size : 52,6 Mb
Release : 1999
Category : Science
ISBN : UOM:39015048512183
Optical Diagnostics for Fluids/heat/combustion and Photomechanics for Solids by Soyoung S. Cha,P. Bryanston-Cross,Carolyn Regan Mercer Pdf
NASA Scientific and Technical Reports
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher : Unknown
Page : 2300 pages
File Size : 53,6 Mb
Release : 1967
Category : Aeronautics
ISBN : STANFORD:36105113793777
NASA Scientific and Technical Reports by United States. National Aeronautics and Space Administration Scientific and Technical Information Division Pdf
A Selected Listing of NASA Scientific and Technical Reports for ...
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher : Unknown
Page : 2088 pages
File Size : 48,8 Mb
Release : 1966
Category : Aeronautics
ISBN : CORNELL:31924057848834
A Selected Listing of NASA Scientific and Technical Reports for ... by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Pdf
Transonic Shock-induced Dynamics of a Flexible Wing with a Thick Circular-arc Airfoil
Author : Anonim
Publisher : Unknown
Page : 16 pages
File Size : 52,9 Mb
Release : 1991
Category : Electronic
ISBN : NASA:31769000595762
Transonic Shock-induced Dynamics of a Flexible Wing with a Thick Circular-arc Airfoil by Anonim Pdf
Aeroelasticity at the NASA Langley Research Center Recent Progress, New Challenges
Author : Anonim
Publisher : Unknown
Page : 80 pages
File Size : 53,9 Mb
Release : 1985
Category : Electronic
ISBN : NASA:31769000572381
Aeroelasticity at the NASA Langley Research Center Recent Progress, New Challenges by Anonim Pdf
A Collection of Technical Papers: Structural dynamics I
Author : Anonim
Publisher : Unknown
Page : 776 pages
File Size : 54,6 Mb
Release : 1991
Category : Aerodynamics
ISBN : UCSD:31822006449458