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AEROSP 315 - Aircraft/Spacecraft Structures
Winter 2022, Section 001
Instruction Mode: Section 001 is   Hybrid (see other Sections below)
Subject: Aerospace Engineering (AEROSP)
Department: CoE Aerospace Engineering
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 Details  Description  Schedule  Textbooks/Other Materials  Syllabi

Details

Credits:
3 (Non-LSA credit).
Requirements & Distribution:
BS
Waitlist Capacity:
unlimited
Advisory Prerequisites:
AEROSP 215 and Math 216.
BS:
This course counts toward the 60 credits of math/science required for a Bachelor of Science degree.
Repeatability:
May not be repeated for credit.
Primary Instructor:
Shaw,John A
Start/End Date:
Full Term 1/5/22 - 4/19/22 (see other Sections below)
NOTE: Drop/Add deadlines are dependent on the class meeting dates and will differ for full term versus partial term offerings.
For information on drop/add deadlines, see the Office of the Registrar and search Registration Deadlines.

Description

Concepts of displacement, strain, stress, compatibility, equilibrium, and constitutive equations as used in solid mechanics. Emphasis is on boundary-value problem formulation via simple examples, followed by the use of the finite-element method for solving problems in vehicle design.

Schedule

AEROSP 315 - Aircraft/Spacecraft Structures
Schedule Listing
001 (LEC)
  Hybrid
10530
Closed
0
 
-
MW 1:30PM - 3:00PM1008 FXB
1/5/22 - 4/19/22

Textbooks/Other Materials

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Syllabi

Syllabi are available to current LSA students. IMPORTANT: These syllabi are provided to give students a general idea about the courses, as offered by LSA departments and programs in prior academic terms. The syllabi do not necessarily reflect the assignments, sequence of course materials, and/or course expectations that the faculty and departments/programs have for these same courses in the current and/or future terms.

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CourseProfile (Atlas)

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