Collection

CoED

Authors

Bryan A Jones; J W Bruce; Mahnas Jean Mohammadi-Aragh

implementations and investigations. Keywords: Literate Programming, Computing Education, Writing OPEN ACCESS Related ASEE Publications Volume 11 [7] J. W. Bruce, B. A. Jones, and M. J. Mohammadi-Aragh. “A Literate Programming Approach for Issue Hardware Description Language Instruction,”. In 2019 ASEE Annual Conference & Exposition. 2 ASEE Conferences, 2019. URL 10.18260/1-2--31966. *Corresponding author [8] B. A. Jones and M. J. Mohammadi-Aragh. “Employing Literate Programming Instruction in a Submitted 1 Aug 2019 Microprocessors Course

Collection

CoED

Authors

Bahaa Ansaf; Neb Jaksic

Students Accepted 7 Oct 20 Using a Project-based Sequential Learning Approach,”. In ASEE Annual Conference Proceedings. Citation ASEE, June 2018. Ansaf B. and Jaksic N.“Simulation and Interactive [12] B. Ansaf and N. Jaksic. “Teaching Undergraduate Manufacturing Course using a Design-based Digital Tools to Support Teaching Approach,”. In ASEE Annual Conference Proceedings. ASEE, June 2019. Teaching Engineering Manufacturing Processes [1] D. Wendell. “Teaching Undergraduate Manufacturing in a Flipped Classroom,”. In and others, Course,” Computers in Education Journal, vol. 11, editor, ASEE Annual Conference and Exposition, Conference Proceedings, June 2018

Collection

CoED

Authors

Mario Perhinschi

: Consider that the aircraft is initially in a steady-state, horizontal, and symmetricflight. At a certain moment, the left elevator is locked at trim. Without any pilot input, the occurrence ofthe failure can. . . (circle one). • a) easily be detected mainly due to the significant pitch rate produced without any other rotation. • b) easily be detected mainly due to the significant roll rate produced without any other rotation. • c) easily be detected mainly due to the significant pitch rate produced coupled with roll rate. • d) easily be detected mainly due to the significant pitch rate produced coupled with yaw rate. • e) not be easily detected.Example question #2: Consider that the aircraft is initially in a steady-state, horizontal