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Preliminary Results from the QuietSpike Flight TestThis viewgraph presentation reviews the QuietSpike flight test results. It shows the previous tests from Nearfield probes. The presentation then reviews the approach to test the QuietSpike, and shows graphics of the positions of the test vehicles. It also shows the components of the Sonic Boom Probing Noseboom. A graph of the Pressure Over- Under-shoot (Shaped Sonic Boom Demonstration (SSBD)Data) is presented. It reviews the Shock Probing Orientations, explaining that the probing plane is always behind the tail of the QuietSpike jet. Graphs of the Shock Position Geometry (SSBD Data) and the QuietSpike signature as of the test on 12/13/06, Near-Field Probing Directly Under the QuietSpike jet, and Near-Field Probing to Side, Near-Field Probing Above and to Side. Several slides review the Computational Fluid Dynamic models, and results compared to the probe tests.
Document ID
20080003864
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Haering, Edward A., Jr.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Cliatt, Larry J., II
(NASA Dryden Flight Research Center Edwards, CA, United States)
Howe, Don
(Gulfstream Aerospace Corp. Bethany, OK, United States)
Waithe, Kenrick
(Gulfstream Aerospace Corp. Bethany, OK, United States)
Date Acquired
August 24, 2013
Publication Date
October 30, 2007
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: Industry Panel Presentation at the University of Southern California
Location: Los Angeles, CA
Country: United States
Start Date: November 3, 2017
Sponsors: University of Southern California
Distribution Limits
Public
Copyright
Public Use Permitted.
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