Accession Number:

AD0609489

Title:

PERFORMANCE FLIGHT TESTING THEORY,

Descriptive Note:

Corporate Author:

AIR FORCE AEROSPACE RESEARCH PILOT SCHOOL EDWARDS AFB CALIF

Report Date:

1964-01-01

Pagination or Media Count:

93.0

Abstract:

Contents The atmosphere Instrumentation Pitot-static system theory Non-steady state performance Turning performance Steady state performance Fuel flow corrections Takeoff and landing theory.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE