Position Error Calibration of a Pressure Survey Aircraft Using a Trailing Cone PDF Download
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Author: Edward N. Brown
Publisher:
ISBN:
Category : Aeronautics in meteorology
Languages : en
Pages : 50
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Book Description
Author: Edward N. Brown
Publisher:
ISBN:
Category : Aeronautics in meteorology
Languages : en
Pages : 50
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1134
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Book Description
Author: Edward N. Brown
Publisher:
ISBN:
Category : Aeronautics in meteorology
Languages : en
Pages : 54
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 524
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Book Description
Author: Frank L. Jordan
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 36
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
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Book Description
Limited flight tests were conducted using the trailing cone static pressure measuring technique to determine the repeatability of commercial jet aircraft altimeter systems. The maximum difference between the six types tested at 30,000 feet was 500 feet.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
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Author: Jack J. Shrager
Publisher:
ISBN:
Category :
Languages : en
Pages : 67
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Book Description
An experimental trail cone stabilized static source system was fabricated and tested using various towing aircraft at speeds up to 1.12 Mach Number to determine its suitability as a 'standard' method for determining altimeter static pressure error. Flight tests were conducted at sea level, 5, 000, 10,000, 15,000, 25,000, 30,000 and 40,000 feet, to determine the static pressure defect of the trailing cone system. Test results indicated that the experimental system had a nominal 'position error' equal to = 12 feet at sea level and = 30 feet at 30,000 feet.
Author:
Publisher:
ISBN:
Category : Atmosphere
Languages : en
Pages : 214
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Book Description
