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Experimental and Computational Study of the X-59 Wind Tunnel Model at Glenn Research Center 8- by 6-foot Supersonic Wind Tunnel The Commercial Supersonics Technology (CST) Project under the NASA Advanced Air
Vehicles Program (AAVP) focuses on developing technologies for enabling designs of future
commercial supersonic aircraft. Many different technology areas are being addressed, such as
designing airframes for better efficiency, improving engine integration for minimizing noise,
maximizing combustion efficiency, and reducing high-altitude emissions, but the greatest
emphasis has been on understanding the contributions to sonic boom loudness and learning how
to shape the airframe and integrate the engine(s) such that the boom noise is minimized.
Document ID
20220011496
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Carter, Melissa B.
(Langley Research Center Hampton, Virginia, United States)
Elmiligui, Alaa A.
(Langley Research Center Hampton, Virginia, United States)
Park, Michael A.
(Langley Research Center Hampton, Virginia, United States)
Shea, Patrick R.
(Langley Research Center Hampton, Virginia, United States)
Winski, Courtney S.
(Langley Research Center Hampton, Virginia, United States)
Durston, Donald A.
(Ames Research Center Mountain View, California, United States)
Jensen, James C.
(Ames Research Center Mountain View, California, United States)
Wagner, Jacob M
(Ames Research Center Mountain View, California, United States)
Neuhoff, Scott M
(Ames Research Center Mountain View, California, United States)
Wolter, John D.
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
July 29, 2022
Publication Date
September 1, 2022
Subject Category
Aerodynamics
Funding Number(s)
WBS: 110076.02.07.03.31
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
CST
X-59
Sonic Boom
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