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CORRECTED THRUST VERSUS ENGINE NOZZLE PRESSURE RATIOFOR TABLE E1 EXAMPLE DATA
标准号：
AIR1678B
标准名称： Uncertainty of In-Flight Thrust Determination
同源图形
MEASUREMENT ERROR, δ
ERROR CLASSIFICATION
MEASUREMENT ERROR CO
NORMAL DISTRIBUTION
SYSTEMATIC ERROR
MEASUREMENT CALIBRAT
EXAMPLE DATA ACQUISI
DISTRIBUTION OFiX AN
SYSTEMATIC STANDARD
RECOMMENDED TABLE FO
RECOMMENDED TABLE FO
FIGURE 11 - GROUND T
GENERAL FLIGHT TEST
EXAMPLE PRELIMINARY
GROUND TEST MEASUREM
IN-FLIGHT THRUST MEA
ILLUSTRATION OF MATH
ILLUSTRATION OF MATH
FLIGHT TEST MEASUREM
TWO-TAILED 95% STUDE
EXAMPLE UNCERTAINTY
GAUSSIAN DISTRIBUTIO
RECTANGULAR DISTRIBU
TRIANGULAR DISTRIBUT
FIGURE 1
相关图形
：BEGIN METAFILE‘Ex
GJBz 20114.3-93
自动化指挥系统图形数
TEMPERATURE – PRESSU
AIR1059C
(R) Oxygen
FIGURE 1. Typical To
AIR1087B
Aircraft A
FIGURE 3 - Torque Ve
AIR1087B
Aircraft A
FIGURE 4 - Torque Ve
AIR1087B
Aircraft A
FIGURE 6 - Torque Ve
AIR1087B
Aircraft A
FIGURE 7 - Y Versus
AIR1087B
Aircraft A
FIGURE 9 - Torque Ve
AIR1087B
Aircraft A
FIGURE 10 - Viscosit
AIR1087B
Aircraft A
Specific Optical Den
AIR1106A
Some Facto