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{ "item_title" : "Assessing the Potential for Improved Scramjet Performance Through Application of Electromagnetic Flow Control", "item_author" : [" Martin Forrester Lindsey "], "item_description" : "Sustained hypersonic flight using scramjet propulsion is the key technology bridging the gap between turbojets and the exoatmospheric environment where a rocket is required. Recent efforts have focused on electromagnetic (EM) flow control to mitigate the problems of high thermomechanical loads and low propulsion efficien- cies associated with scramjet propulsion. This research effort is the first flight-scale, three-dimensional computational analysis of a realistic scramjet to determine how EM flow control can improve scramjet performance. Development of a quasi-one dimen- sional design tool culminated in the first open source geometry of an entire scramjet flowpath. This geometry was then tested extensively with the Air Force Research Laboratory's three-dimensional Navier-Stokes and EM coupled computational code.", "item_img_path" : "https://covers3.booksamillion.com/covers/bam/1/28/833/513/128833513X_b.jpg", "price_data" : { "retail_price" : "18.95", "online_price" : "18.95", "our_price" : "18.95", "club_price" : "18.95", "savings_pct" : "0", "savings_amt" : "0.00", "club_savings_pct" : "0", "club_savings_amt" : "0.00", "discount_pct" : "10", "store_price" : "" } }
Assessing the Potential for Improved Scramjet Performance Through Application of Electromagnetic Flow Control|Martin Forrester Lindsey

Assessing the Potential for Improved Scramjet Performance Through Application of Electromagnetic Flow Control

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Overview

Sustained hypersonic flight using scramjet propulsion is the key technology bridging the gap between turbojets and the exoatmospheric environment where a rocket is required. Recent efforts have focused on electromagnetic (EM) flow control to mitigate the problems of high thermomechanical loads and low propulsion efficien- cies associated with scramjet propulsion. This research effort is the first flight-scale, three-dimensional computational analysis of a realistic scramjet to determine how EM flow control can improve scramjet performance. Development of a quasi-one dimen- sional design tool culminated in the first open source geometry of an entire scramjet flowpath. This geometry was then tested extensively with the Air Force Research Laboratory's three-dimensional Navier-Stokes and EM coupled computational code.

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Details

  • ISBN-13: 9781288335138
  • ISBN-10: 128833513X
  • Publisher: Biblioscholar
  • Publish Date: November 2012
  • Dimensions: 9.21 x 6.14 x 0.38 inches
  • Shipping Weight: 0.57 pounds
  • Page Count: 178

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