Investigation at Supersonic Speeds of the Compressor Stall and Inlet Buzz Characteristics of a J34 - Spike-inlet Combination PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Investigation at Supersonic Speeds of the Compressor Stall and Inlet Buzz Characteristics of a J34 - Spike-inlet Combination PDF full book. Access full book title Investigation at Supersonic Speeds of the Compressor Stall and Inlet Buzz Characteristics of a J34 - Spike-inlet Combination by J. Cary Nettles. Download full books in PDF and EPUB format.
Author: J. Cary Nettles Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 34
Book Description
For a Mach number range from 1.6 to 2.0 and angles of attack from 0 to 9 degrees the occurrence of stall was related to the presence of a pressure deficiency at the hub of the compressor. The referred engine air flow tended to increase as radial distortion level increased. Approaching the inlet buzz limit with the engine operating in or near a stall condition did not affect the minimum stable air flow of the diffuser, and conversely the presence of mild buzz did not affect the compressor stall limit. The stability limits of a 15 degree plus 10 degree double-cone inlet were essentially the same with the engine as with a choked plug.
Author: J. Cary Nettles Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 34
Book Description
For a Mach number range from 1.6 to 2.0 and angles of attack from 0 to 9 degrees the occurrence of stall was related to the presence of a pressure deficiency at the hub of the compressor. The referred engine air flow tended to increase as radial distortion level increased. Approaching the inlet buzz limit with the engine operating in or near a stall condition did not affect the minimum stable air flow of the diffuser, and conversely the presence of mild buzz did not affect the compressor stall limit. The stability limits of a 15 degree plus 10 degree double-cone inlet were essentially the same with the engine as with a choked plug.
Author: Clifford J. Moore Publisher: ISBN: Category : Aeronautics Languages : en Pages : 492
Book Description
This report investigates critical reviews of NACA and NASA report literature on light aircraft design, with emphasis on propulsion subsystems, stability, control, propellers, performance, and safety.
Author: J. Cary Nettles
Author: J. Cary Nettles
Author: United States. Superintendent of Documents
Author: United States. National Aeronautics and Space Administration
Author: David N. Bowditch
Author: Daniel W. Lester
Author: Clifford J. Moore
Author: United States. National Aeronautics and Space Administration
Author: Edward Przebienda
Author: 
Author: Clifford J. Moore