ANN's Daily Aero-Term (02.07.09): S-Duct | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-05.06.24

Airborne-NextGen-05.07.24

Airborne-Unlimited-05.08.24 Airborne-FlightTraining-05.09.24

Airborne-Unlimited-05.10.24

Sat, Feb 07, 2009

ANN's Daily Aero-Term (02.07.09): S-Duct

Aero-Terms!

Aero-Terms are designed to be a daily reminder of the terms, names, acronyms and explanations of the unique language that populates the aviation world. Aerospace, sport aviation, fixed wing, helo, you name it... it's all fair game.

Aero-Terms should serve as a quick but intriguing reminder of the terms you may use every day, or an introduction to an aspects of the Aero-World you may not yet be familiar with. ANN also encourages readers to go beyond the FMI link, and further research any intriguing terms.

Suggestions for future Aero-Terms are ALWAYS welcome, as are additions or discussion of the explanations given for each Aero-Term.

S-Duct

An S-duct is a unique type of jet engine intake duct, used only on trijets. The S-duct is located in the tail, or empennage, of the aircraft. As well, the shape of the S-duct is distinctive and easily recognized.  The S-duct was invented as a solution for positioning the central engine on trijets. The S-duct was easier to service that alternative trijet designs.[1] Most trijet designs opted for the S-duct layout. In fact, only the DC-10 and MD-11 trijets chose not to use the S-duct and go with a straight-through layout. The straight-through layout leaves the engine high above the ground, making access difficult. The straight layout also increases total aircraft drag by 2-4%. On the L-1011, engineers were able to maintain "straight-thru" engine performance by limiting the curve of the S-duct to less than 25% of the radius of the engine intake diameter. The S-duct design also reduced the total empty aircraft weight.

FMI: www.ara.co.uk/content/2/160/s-duct.html

Advertisement

More News

Airborne-Flight Training 05.09.24: ERAU at AIAA, LIFT Diamond Buy, Epic A&P

Also: Vertical Flight Society, NBAA Maintenance Conference, GA Honored, AMT Scholarship For the first time, students from Embry-Riddle’s Daytona Beach, Florida, campus took t>[...]

ANN's Daily Aero-Term (05.07.24): Hazardous Weather Information

Hazardous Weather Information Summary of significant meteorological information (SIGMET/WS), convective significant meteorological information (convective SIGMET/WST), urgent pilot>[...]

Aero-News: Quote of the Day (05.07.24)

"The need for innovation at speed and scale is greater than ever. The X-62A VISTA is a crucial platform in our efforts to develop, test and integrate AI, as well as to establish AI>[...]

NTSB Final Report: Cessna 150

(FAA) Inspector Observed That Both Fuel Tanks Were Intact And That Only A Minimal Amount Of Fuel Remained In Each Analysis: According to the pilot, approximately 8 miles from the d>[...]

Aero-News: Quote of the Day (05.08.24)

“Pyka’s Pelican Cargo is unlike any other UAS solution on the market for contested logistics. We assessed a number of leading capabilities and concluded that the Pelica>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC