The objective of the refan program is to demonstrate the technical feasibility of substantially reducing the noise levels of existing JT8D powered aircraft. The program consists of the design, manufacturing and testing of the refan engines and modified nacelles and airplanes. Experimental testing was completed for the refan engine both at sea level and at altitude conditions. Ground testing for the B727 side- and center-engine installations and flight testing of the DC-9 with refan engines and acoustic nacelles were performed. Preliminary results presented show that substantial noise reductions were achieved
The refan JT8D-109 performance and stability characteristics are reported as determined from sea lev...
This final report has been prepared by Honeywell Aerospace, Phoenix, Arizona, a unit of Honeywell In...
Efforts to develop an engine noise reduction technology suitable for use on subsonic and conventiona...
The Refan Program is aimed at a large reduction in aircraft approach and takeoff noise in the vicini...
The technical feasibility is described of substantially reducing the noise levels of existing JT8D p...
The retrofit of JT8D-109 (refan) engines are evaluated on a 727-200 airplane in terms of airworthine...
The propulsion performance, acoustic, structural, and systems changes to a 727-200 airplane retrofit...
Analyses and design studies were conducted on the technical and economic feasibility of installing t...
The objective of the JT8D refan program was to design, fabricate, and test certifiable modifications...
The design, analysis, fabrication, and ground and flight testing of DC-9 airframe/nacelle hardware w...
Major airports in the world's air transportation systems face a serious problem in providing greater...
A program to reduce the community noise levels of commercial jet aircraft is summarized. The program...
The results from two low-speed wind tunnel tests of the Boeing 727-200 airplane as configured with t...
This presentation reviews engine noise research conducted at the NASA Glenn Research Center over the...
Flyover noise measurements were made (using Federal Aviation Regulations, part 36 procedures) of two...
The refan JT8D-109 performance and stability characteristics are reported as determined from sea lev...
This final report has been prepared by Honeywell Aerospace, Phoenix, Arizona, a unit of Honeywell In...
Efforts to develop an engine noise reduction technology suitable for use on subsonic and conventiona...
The Refan Program is aimed at a large reduction in aircraft approach and takeoff noise in the vicini...
The technical feasibility is described of substantially reducing the noise levels of existing JT8D p...
The retrofit of JT8D-109 (refan) engines are evaluated on a 727-200 airplane in terms of airworthine...
The propulsion performance, acoustic, structural, and systems changes to a 727-200 airplane retrofit...
Analyses and design studies were conducted on the technical and economic feasibility of installing t...
The objective of the JT8D refan program was to design, fabricate, and test certifiable modifications...
The design, analysis, fabrication, and ground and flight testing of DC-9 airframe/nacelle hardware w...
Major airports in the world's air transportation systems face a serious problem in providing greater...
A program to reduce the community noise levels of commercial jet aircraft is summarized. The program...
The results from two low-speed wind tunnel tests of the Boeing 727-200 airplane as configured with t...
This presentation reviews engine noise research conducted at the NASA Glenn Research Center over the...
Flyover noise measurements were made (using Federal Aviation Regulations, part 36 procedures) of two...
The refan JT8D-109 performance and stability characteristics are reported as determined from sea lev...
This final report has been prepared by Honeywell Aerospace, Phoenix, Arizona, a unit of Honeywell In...
Efforts to develop an engine noise reduction technology suitable for use on subsonic and conventiona...