Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722890629
Category :
Languages : en
Pages : 26
Book Description
A technique is presented for the calibration of a hemispherical tipped 0.125 inch diameter 5-hole probe. The derivation of equations from the potential flow over a sphere relating the flow angle and velocity to pressure differentials measured by the probe is presented. The technique for acquiring the calibration data and the technique used to calculate the calibration coefficients are presented. The accuracy of the probe in both the uniform calibration flow field and the nonuniform flow field over a 75 degree swept delta wing is discussed. Kjelgaard, Scott O. Langley Research Center RTOP 505-60-11-03...
Theoretical Derivation and Calibration Technique of a Hemispherical-Tipped, Five-Hole Probe
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722890629
Category :
Languages : en
Pages : 26
Book Description
A technique is presented for the calibration of a hemispherical tipped 0.125 inch diameter 5-hole probe. The derivation of equations from the potential flow over a sphere relating the flow angle and velocity to pressure differentials measured by the probe is presented. The technique for acquiring the calibration data and the technique used to calculate the calibration coefficients are presented. The accuracy of the probe in both the uniform calibration flow field and the nonuniform flow field over a 75 degree swept delta wing is discussed. Kjelgaard, Scott O. Langley Research Center RTOP 505-60-11-03...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722890629
Category :
Languages : en
Pages : 26
Book Description
A technique is presented for the calibration of a hemispherical tipped 0.125 inch diameter 5-hole probe. The derivation of equations from the potential flow over a sphere relating the flow angle and velocity to pressure differentials measured by the probe is presented. The technique for acquiring the calibration data and the technique used to calculate the calibration coefficients are presented. The accuracy of the probe in both the uniform calibration flow field and the nonuniform flow field over a 75 degree swept delta wing is discussed. Kjelgaard, Scott O. Langley Research Center RTOP 505-60-11-03...
Theoretical Derivation and Calibration Technique of a Hemispherical-tipped, Five-hole Probe
Author: Scott O. Kjelgaard
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Book Description
Scientific and Technical Aerospace Reports
NASA Technical Memorandum
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 882
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 882
Book Description
In-flight Leading-edge Extension Vortex Flow-field Survey Measurements on a F-18 Aircraft at High Angle of Attack
Author: David M. Richwine
Publisher:
ISBN:
Category : Research aircraft
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category : Research aircraft
Languages : en
Pages : 56
Book Description
12th AIAA Applied Aerodynamics Conference
NASA SP.
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1300
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1300
Book Description