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1 edition of An investigation of a prototype OASYS" effectiveness in maneuvering flight found in the catalog.

An investigation of a prototype OASYS" effectiveness in maneuvering flight

Christopher Cyril Sullivan

An investigation of a prototype OASYS" effectiveness in maneuvering flight

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  • 18 Currently reading

Published by Naval Postgraduate School, Available from the National Technical Information Service in Monterey, Calif, Springfield, Va .
Written in English


Edition Notes

ContributionsWood, E. Roberts
The Physical Object
Pagination148 p. ;
Number of Pages148
ID Numbers
Open LibraryOL25454446M


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An investigation of a prototype OASYS" effectiveness in maneuvering flight by Christopher Cyril Sullivan Download PDF EPUB FB2

An Investigation of a Prototype OASYS' Effectiveness in Maneuvering Flight by Christopher Cyril Sullivan Captain, United States Army B.S., United States Military Academy (West Point, NY), Submitted in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE IN AERONAUTICAL ENGINEERING from the NAVAL POSTGRADUATE SCHOOL.

An investigation of a prototype OASYS effectiveness in maneuvering flight book for public release; distribution is unlimitedAn analysis of the current Northrop helicopter obstacle avoidance system (OASYS) An investigation of a prototype OASYS effectiveness in maneuvering flight book with a fixed forward mounting, 25 x 50 degree field of view, nanometer wavelength LADAR, was conducted to determine system effectiveness during simulated aircraft level accelerations ranging from 0 to Author: Christopher Cyril Sullivan.

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An Experimental Investigation of the Transient Effects Associated with Wing Deployment During Ballistic Flight Mortar weapons systems have existed for more than five hundred years.

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Dole, James E. Lewis, Joseph R. Badick, Brian A. Johnson, Charles E. (Institute Of Safety, Systems Management Hardcover, Pages, Published ISBN / ISBN / Book Edition: 3rd Edition. Phase-locked Planar PIV measurements were performed in the pdf of the flapping wing model, as seen in Fig.

1 to investigate the pdf behavior in the wake of the flapping wing. One CCD camera (labeled with Cam 1 in Fig. 1) is employed and positioned perpendicularly to the laser sheet and equipped with a 50 mm Nikon field of view under investigation was Cited by: 1.Manned Simulation Study Results Concerning Design Parameters for an Effective Helicopter Obstacle Avoidance System OASYS Paper presented at the AHS International Fo VFS WebsiteCited by: [email protected]{osti_, title = {ICAS, Congress, 16th, Jerusalem, Ebook, Aug.

Sept. 2,Proceedings. Volumes 1 and 2}, author = {Not Available}, abstractNote = {The present conference discusses topics in aircraft environmental safety, hypersonic aerothermodynamics, fatigue and damage tolerance, laminar flow regimes, the application of CFD to propulsion, helicopter flight .