Design Studies and Model Tests of the Stowed Tilt Rotor Concept. Volume III. Appendixes

Abstract

This Appendix contains a description of the drag prediction methodology used in this study, minimum parasite drag breakdowns for all the point design aircraft, and detailed performance data for the Design Point 1, 2, and 3 aircraft.(

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1971
Accession Number
AD0729429

Entities

People

  • Bernard L. Fry

Organizations

  • Boeing Rotorcraft Systems

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Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Fixed Wing Aircraft
  • Governments
  • Mach Number
  • Short Takeoff Aircraft
  • Three Dimensional
  • Tilt Rotor Aircraft
  • Transport Aircraft
  • Vehicles
  • Vertical Takeoff Aircraft

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