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Question 1 The thrust of a jet turbine engine is thought to be related to the primary speed of rotation (X1), the secondary speed of rotation (X2), the fuel flow rate (X3), the pressure (X4), and the temperature(X5) Find an upper bound on the mean thrust Usa alpha 0 05, n-20, MSE-1 and assume the covariance matrix is an identity ((XTx)1-1] Predictor Cuef x0 Constant -2.25 053 28 41 x2 0.20 15.09 x3 -0.16 13.78 x4 -0.025 19.02 -0 325 15 46 Selected Answer oc. 98 62 Corroct Answor. O a. 84 59 I think the "correct answer" is not really correct. Can you check this?

Question 1 The thrust of a jet turbine engine is thought to be related to the primary speed of rotation (X1), the secondary speed of rotation (X2), the fuel flow rate (X3), the pressure (X4), and the temperature(X5) Find an upper bound on the mean thrust Usa alpha 0 05, n-20, MSE-1 and assume the covariance matrix is an identity ((XTx)1-1] Predictor Cuef x0 Constant -2.25 053 28 41 x2 0.20 15.09 x3 -0.16 13.78 x4 -0.025 19.02 -0 325 15 46 Selected Answer oc. 98 62 Corroct Answor. O a. 84 59 I think the "correct answer" is not really correct. Can you check this?

MATLAB: An Introduction with Applications
MATLAB: An Introduction with Applications
6th Edition
ISBN:9781119256830
Author:Amos Gilat
Publisher:Amos Gilat
Chapter1: Starting With Matlab
Section: Chapter Questions
Problem 1P
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Question 1 The thrust of a jet turbine engine is thought to be related to the primary speed of rotation (X1), the secondary speed of rotation (X2), the fuel flow rate (X3), the pressure (X4), and the temperature(X5). Find an upper bound on the mean thrust Usa alpha 0 05, n-20, MSE=1 and assume the covariance matrix is an identity [(XTx)1-1] Predictor Cuef x0 Constant -2.25 053 28 41 x2 0.20 15.09 x3 -0.16 13.78 x4 -0.025 19.02 -0 325 15 46 Selected Answer oc. 98 62 Corroct Answor. O a. 84 59 I think the "correct answer" is not really correct. Can you check this?
Transcribed Image Text:Question 1 The thrust of a jet turbine engine is thought to be related to the primary speed of rotation (X1), the secondary speed of rotation (X2), the fuel flow rate (X3), the pressure (X4), and the temperature(X5). Find an upper bound on the mean thrust Usa alpha 0 05, n-20, MSE=1 and assume the covariance matrix is an identity [(XTx)1-1] Predictor Cuef x0 Constant -2.25 053 28 41 x2 0.20 15.09 x3 -0.16 13.78 x4 -0.025 19.02 -0 325 15 46 Selected Answer oc. 98 62 Corroct Answor. O a. 84 59 I think the "correct answer" is not really correct. Can you check this?
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