THE DETERMINATION OF HELICOPTER LOGITUDINAL STABILITY DERIVATIVES FROM FLIGHT TEST DATA. PART I. DEVELOPMENT OF FLIGHT TEST INSTRUMENTATION. TECHNIQUES AND ANALYSIS METHODS

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1958
Accession Number
AD0110443

Entities

People

  • E.r. Schultz
  • W.r. Deazley

Organizations

  • Calspan

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Helicopters
  • Instrumentation
  • Rotary Wing Aircraft