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Accuracy of Airspeed Measurements and Flight Calibration Procedures

Accuracy of Airspeed Measurements and Flight Calibration Procedures PDF Author: Wilber B. Huston
Publisher:
ISBN:
Category : Air speed
Languages : en
Pages : 88

Book Description
This report reviews in detal the sources of error that may enter into the measurement of airspeed by pitot-static methods. Methods of flight calibration of airspeed installations are given. Special attention is given to the problem of accurate measurement of Mach number, air temperature, and true airspeed during high-speed maneuvers. This report also contains an extensive bibliography.

Accuracy of Airspeed Measurements and Flight Calibration Procedures

Accuracy of Airspeed Measurements and Flight Calibration Procedures PDF Author: Wilber B. Huston
Publisher:
ISBN:
Category : Air speed
Languages : en
Pages : 88

Book Description
This report reviews in detal the sources of error that may enter into the measurement of airspeed by pitot-static methods. Methods of flight calibration of airspeed installations are given. Special attention is given to the problem of accurate measurement of Mach number, air temperature, and true airspeed during high-speed maneuvers. This report also contains an extensive bibliography.

Flight Calibration of Four Airspeed Systems on a Swept-wing Airplane at Mach Numbers Up to 1.04 by the NACA Radar-phototheodolite Method

Flight Calibration of Four Airspeed Systems on a Swept-wing Airplane at Mach Numbers Up to 1.04 by the NACA Radar-phototheodolite Method PDF Author: Jim Rogers Thompson
Publisher:
ISBN:
Category : Air-speed indicators
Languages : en
Pages : 46

Book Description
Of the systems investigated, a nose-boom installation was found to be most suitable for research use at transonic and low supersonic speeds because it provided the greatest sensitivity of the indicated Mach number to a unit change in true Mach number at very high subsonic speeds, and because it was least sensitive to changes in airplane normal-force coefficient. The static-pressure error of the nose-boom system was small and constant above a Mach number of 1.03 after passage of the fuselage bow shock wave over the airspeed head.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1136

Book Description


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Atmospheric Technology PDF Author:
Publisher:
ISBN:
Category : Meteorology
Languages : en
Pages : 712

Book Description


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Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36

Book Description


Report - National Advisory Committee for Aeronautics

Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 760

Book Description


Annual Report of the National Advisory Committee for Aeronautics

Annual Report of the National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
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Pages : 872

Book Description


Technical Note

Technical Note PDF Author:
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Measurement of Aircraft Speed and Altitude PDF Author: William Gracey
Publisher: John Wiley & Sons
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 288

Book Description