EFFECTS OF STRUCTURAL FLEXIBILITY ON GUST LOADING OF AIRCRAFT. PART 2. DYNAMIC STRESSES IN SWEPT-WING AIRPLANES

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1955
Accession Number
AD0078081

Entities

People

  • A.a. Kirsch
  • J.m. Calligeros
  • K.a. Foss

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Wings
  • Aircrafts
  • Airframes
  • Airplanes
  • Fixed Wing Aircraft
  • Resilience
  • Swept Wings
  • Vehicles