Measurement of Aircraft Speed and Altitude PDF Download
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Author: William Gracey
Publisher: John Wiley & Sons
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 288
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Book Description
Author: William Gracey
Publisher: John Wiley & Sons
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 288
Get Book Here
Book Description
Author: William Gracey
Publisher: John Wiley & Sons
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 288
Get Book Here
Book Description
Author: Wendell H. Stillwell
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 16
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Book Description
Author: William Gracey
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 44
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Book Description
Author: Wendell H. Stillwell
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22
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Book Description
On August 4, 1960, a flight was made with the X-15 airplane to the maximum speed expected with the interim rocket engines. Fully corrected airspeed measurements showed that the maximum Mach number of 3/31 +/-0.04 and maximum true airspeed of 2,196 mph +/- 35 were attained at an altitude of 69,600 feet. At Mach numbers greater than 2.0 the pitot-static tube exhibited a negative static-pressure error which resulted in a Mach number correction of -0.18 at the maximum speed.
Author: G. G. Readett
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Book Description
Aircraft Research and Development Unit has developed a trailing pitot-static probe suitable for determining pressure error corrections for aircraft airspeed and altitude systems. The instrument is suitable for use with helicopters where both pitot and static pressure measurements on the aircraft could be subject to pressure errors due to rotor downwash. The probe is accurate to better than 1% and was tested and shown to be satisfactory over a speed range of 40 to 120 knots. (Author).
Author: Steve L. Swihart
Publisher:
ISBN:
Category :
Languages : en
Pages : 280
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Book Description
Author: Wilber B. Huston
Publisher:
ISBN:
Category : Air speed
Languages : en
Pages : 88
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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.
Author: William Gracey
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: F. L. Thompson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 16
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Book Description
Various methods of measuring the air speed of airplanes are described. Particular emphasis is placed on the procedure required to obtain precise measurements of speed by the use of the suspended pitot-static head or the suspended static head. Typical calibration curves for service installations of pitot-static heads are shown and the relation between errors in air speed and corresponding errors in observed altitude for such installations is discussed. There is included a brief discussion of various speed-course methods of measuring speed.
