Accession Number : ADA320220

Title :   Volume 1. Performance Flight Testing Phase. Chapter 2. Subsonic Aerodynamics.

Corporate Author : AIR FORCE TEST PILOT SCHOOL EDWARDS AFB CA

PDF Url : ADA320220

Report Date : NOV 1992

Pagination or Media Count : 130

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.

Descriptors :   *FLIGHT TESTING, *PERFORMANCE(ENGINEERING), *SUBSONIC CHARACTERISTICS, *COURSES(EDUCATION), *AERODYNAMICS, BOUNDARY LAYER, AIRFOILS, SWEPT WINGS, PROFILES, FLIGHT ENVELOPE, MACH NUMBER, HIGH LIFT, VOCABULARY, EQUATIONS, DRAG, WINGS, VISCOUS FLOW, ACOUSTIC VELOCITY, ATMOSPHERES, SKIN FRICTION, COMPRESSIVE PROPERTIES.

Subject Categories : Aerodynamics
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      Mfg & Industrial Eng & Control of Product Sys
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE