Low Speed Rot Or/Fuselage Interactional Aerodynamics

By: Nasa, National Aeronautics and Space Adm

This report presents work performed under a Cooperative Research Agreement between Virginia Tech and the NASA Langley Research Center. The work involved development of computational techniques for modeling helicopter rotor/airframe aerodynamic interaction. A brief overview of the problem is presented, the modeling techniques are described, and selected example calculations are briefly discussed.Barnwell, Richard W. and Prichard, Devon S.Langley Research CenterCOMPUTER PROGRAMS; MODELS; ROTOR BODY INTERACTIONS; INTERACTIONAL AERODYNAMICS; FUSELAGES; AIRFRAMES

• Format: Paperback
• Language: English
• ISBN: 1723736902
• ISBN13: 9781723736902
• Release Date: January 1
• Publisher: Independently Published
• Length: 40 Pages
• Weight: 0.26 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"