Determination of Quantitative Relationships between Selected Critical Helicopter Design Parameters.

Abstract

This thesis determines the relationships of helicopter design parameters by first depicting graphically all possible pairings of selected design parameter values and then, secondly, depicting graphically respective curve fits for the data point plots which meet an acceptance criteria. In generating the curve plots, the specific constants of each curve equation are determined, thus allowing the designer the ability to derive quantitatively the values of many of the design parameters heretofore selected by trial and error methods. Originator-supplied keywords include: Quantitative Relationships of Helicopter Design Parameters.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1984
Accession Number
ADA152034

Entities

People

  • R. S. Petricka

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Army Aviation
  • Attack Helicopters
  • Blades
  • California
  • Computer Programs
  • Databases
  • Ground Effect
  • Helicopters
  • Ions
  • Observation Aircraft
  • Plastic Explosives
  • Tail Rotors
  • United States

Readers

  • Regression Analysis.