Repository logo
Log In(current)
  1. Home
  2. Colleges & Schools
  3. Graduate School
  4. Masters Theses
  5. Application of the MCA method to determine in-flight drag of a propeller driven aircraft
Details

Application of the MCA method to determine in-flight drag of a propeller driven aircraft

Date Issued
May 1, 1990
Author(s)
Gibby, John K.
Advisor(s)
R. D. Kimberlin
Additional Advisor(s)
Charles Limbaugh, William Baker Jr
Abstract

The Mass Consumption Acceleration (MCA) method has been used successfully to determine the in-flight drag of a jet aircraft with fixed area nozzles. The purpose of this study was to apply the method to an aircraft with a reciprocating engine turning a constant speed propeller. The aircraft and engine were modeled with a computer program to generate simulated flight test data. The data were then analyzed with the MCA method. The method is shown to be both theoretically and analytically valid for application to a propeller driven aircraft.

Degree
Master of Science
Major
Aerospace Engineering
File(s)
Thumbnail Image
Name

Thesis90.G522.pdf_AWSAccessKeyId_AKIAYVUS7KB2IXSYB4XB_Signature_94zZHCTaYT1PRhdPaGNq8tGDQWQ_3D_Expires_1736366682

Size

2.28 MB

Format

Unknown

Checksum (MD5)

32dc7e1ff65ee32662a0d42edd7c074a

Built with DSpace-CRIS software - Extension maintained and optimized by 4Science

  • Privacy policy
  • End User Agreement
  • Send Feedback
  • Contact
  • Libraries at University of Tennessee, Knoxville
Repository logo COAR Notify