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BOUNDARY LAYER CONTROL SYSTEM; PRESSURE

contributor authorNAVY - AS - Naval Air Systems Command
date accessioned2017-09-04T18:37:45Z
date available2017-09-04T18:37:45Z
date copyright04/04/1966
date issued1966
identifier otherJODPDAAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsessionid=CA5893FD081D20689A53733F877BE14C/handle/yse/219576
description abstractThis specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff. Intended Use: The boundary layer control system is intended for use in turbo-jet and turbo-prop aircraft to increase the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.
languageEnglish
titleMIL-B-81366num
titleBOUNDARY LAYER CONTROL SYSTEM; PRESSUREen
typestandard
page6
statusActive
treeNAVY - AS - Naval Air Systems Command:;1966
contenttypefulltext


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