Volume 1. Performance Flight Testing Phase. Chapter 2. Subsonic Aerodynamics.
Abstract
Contents include: Fundamental Thoughts and Introduction to the Standard Atmosphere; Basic Aerodynamics I (Governing Equations, Speed of Sound, Mach Number, and Aerodynamic Flight Regimes), Basic Aerodynamics II (Intro to Viscous Flow, Boundary Layer Concepts, Skin Friction Drag and Transition); Basic Aerodynamics III (Pressure and Profile Drag), Airfoil Terminology; Compressibility Effects; Finite Wings, Swept Wings and High Lift Devices; Aircraft Performance I; Intro to Aircraft Performance II.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1992
- Accession Number
- ADA320220