Skip to main content
WebsitebeginnerFree

NASA Glenn Research Center - Beginner's Guide to Aerodynamics

Unknown

NASA Glenn's hypertext guide to flight physics, with short pages on lift, drag, airfoil geometry and the governing equations, each paired with an interactive simulator. Builds intuition before you meet the formal derivations.

Visit resource

More resources on Aerodynamics

WebsiteFree

nasa.gov

NASA.gov is the official site of the U.S. space agency, offering mission news, research results, data, and STEM education resources. It features engineering articles, technical briefs, simulations, multimedia, and classroom materials for students and educators.

WebsiteFree

UIUC Airfoil Coordinates Database

Michael Selig's University of Illinois archive of coordinate files for well over a thousand airfoil sections, downloadable as plain text. Use it to feed real geometry into XFOIL, CFD meshes, or wind-tunnel model design.

CourseFree

Introduction to Aerodynamics (MITx 16.101x)

Video lectures and graded exercises on control-volume conservation of mass and momentum, aerodynamic force coefficients, and isentropic and quasi-one-dimensional compressible flow. Learners finish able to estimate lift, drag and cruise performance for subsonic, transonic and supersonic aircraft.

BookPaid

Fundamentals of Aerodynamics

Anderson's standard undergraduate text, building from the governing conservation equations through incompressible airfoil and finite-wing theory to compressible and supersonic flow. Expect to work problems by hand and read the historical asides.

WebsiteFree

aiaa.org

American Institute of Aeronautics and Astronautics (AIAA) is a professional society for aerospace engineers and students. The site provides industry news, research publications (journals and conference proceedings), standards, education resources, events, and career tools for learning and advancing in aerospace engineering.

BookPaid

Aerodynamics for Engineers

Undergraduate aerospace text pairing classical theory with experimental data and computational practice, covering incompressible flow, boundary layers, and supersonic and hypersonic regimes. Emphasises applying methods to real aircraft configurations rather than derivation alone.

See all Aerodynamics resources →