EFFECTS OF STRUCTURAL FLEXIBILITY ON GUST LOADING OF AIRCRAFT. PART I. GUST LOADS ON SWEPT-WING AIRPLANES FREE TO PITCH AND TO DEFORM STATICALLY

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1955
Accession Number
AD0084480

Entities

People

  • K.a. Foss

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Airplanes
  • Fixed Wing Aircraft
  • Gust Loads
  • Gusts
  • Resilience
  • Swept Wings
  • Vehicles