METHODS OF SELECTION AND APPROXIMATE CALCULATION OF AIR DESIGN PARAMETERS

Abstract

Specific problems in aicraft design are studied. They include airspeed determination of supesonic aircraft; seleion of optimum number of turbojet engines; determination of fuselage slendernessratio; wing weight determination; determination of the parameters of brake assembly design; aircraft trim deterinations for aircraft wth tricycle landing gear; determination of the type and calculation of the rigidity of the trutural stiffening system. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 27, 1962
Accession Number
AD0287668

Entities

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Doors
  • Aircrafts
  • Airframes
  • Airspeed
  • Assembly
  • Engines
  • Fuselages
  • Jet Aircraft
  • Landing Gear
  • Mechanical Structure
  • Rigidity
  • Stiffening
  • Turbojet Engines

Readers

  • Aerospace Engineering
  • Mechanical Engineering/Mechanics of Materials.