Local Flow Conditions for Propulsion Experiments on the NASA F-15B Propulsion Flight Test Fixture

By: Administration (Nasa), National Aeronaut

Local flow conditions were measured underneath the National Aeronautics and Space Administration F-15B airplane to support development of future experiments on the Propulsion Flight Test Fixture (PFTF). The local Mach number and flow angles were measured using a conventional air data boom on a cone-cylinder mounted under the PFTF and compared with the airplane air data nose boom measurements. At subsonic flight speeds, the airplane and PFTF Mach numbers...

• Format: Paperback
• Language: English
• ISBN: B08F6DJ6PW
• ISBN13: 9798672737003
• Release Date: January 1
• Publisher: Independently Published
• Length: 34 Pages
• Weight: 0.23 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"