Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description
Residual Interference Assessment in Adaptive Wall Wind Tunnels
Author: Residual Interference Assessment in Adaptive Wall Wind Tunnels
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722735487
Category :
Languages : en
Pages : 32
Book Description
A two-variable method is presented which is suitable for on-line calculation of residual interference in airfoil testing in the Langley 0.3-Meter Transonic Cryogenic Tunnel (0.3-M TCT). The method applies the Cauchy's integral formula to the closed contour formed by the contoured top and bottom walls, and the upstream and downstream ends. The measured top and bottom wall pressures and position are used to calculate the correction to the test Mach number and the airfoil angle of attack. Application to specific data obtained in the 0.3-M TCT adaptive wall test section demonstrates the need to assess residual interference to ensure that the desired level of wall streamlining is achieved. A FORTRAN computer program was developed for on-line calculation of the residual corrections during airfoil tests in the 0.3-M TCT. Murthy, A. V. Unspecified Center NAS1-18585; RTOP 505-61-01-09...
Residual Interference Assessment in Adaptive Wall Wind Tunnels
Author: National Aeronautics and Space Administration NASAPublisher:
ISBN: 9781728900810
Category :
Languages : en
Pages : 32
Book Description
A two-variable method is presented which is suitable for on-line calculation of residual interference in airfoil testing in the Langley 0.3-Meter Transonic Cryogenic Tunnel (0.3-M TCT). The method applies the Cauchy's integral formula to the closed contour formed by the contoured top and bottom walls, and the upstream and downstream ends. The measured top and bottom wall pressures and position are used to calculate the correction to the test Mach number and the airfoil angle of attack. Application to specific data obtained in the 0.3-M TCT adaptive wall test section demonstrates the need to assess residual interference to ensure that the desired level of wall streamlining is achieved. A FORTRAN computer program was developed for on-line calculation of the residual corrections during airfoil tests in the 0.3-M TCT. Murthy, A. V. Unspecified Center NAS1-18585; RTOP 505-61-01-09...
A Study of Residual Interference Effects in Adaptive Wall Testing of a 7-inch Chord CAST-10-2/DOA 2 Airfoil Model
Author: A. V. MurthyPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 68
Book Description
Scientific and Technical Aerospace Reports
Author: Wind Tunnel Wall Interference (January 1980-May 1988)
Author: Marie H. TuttlePublisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 96
Book Description
NASA Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 80
Book Description
Aerodynamic Characteristics and Pressure Distributions for an Executive-jet Baseline Airfoil Section
Author: Dennis O. AllisonPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 112
Book Description
Transonic Symposium: Theory, Application, and Experiment
Author: Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 964
Book Description
Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1200
Book Description