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A Loudness Calculation Procedure Applied to Shaped Sonic Booms

A Loudness Calculation Procedure Applied to Shaped Sonic Booms PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724999931
Category :
Languages : en
Pages : 32

Book Description
Described here is a procedure that can be used to calculate the loudness of sonic booms. The procedure is applied to a wide range of sonic booms, both classical N-waves and a variety of other shapes of booms. The loudness of N-waves is controlled by overpressure and the associated rise time. The loudness of shaped booms is highly dependent on the characteristics of the initial shock. A comparison of the calculated loudness values indicates that shaped booms may have significantly reduced loudness relative to N-waves having the same peak overpressure. This result implies that a supersonic transport designed to yield minimized sonic booms may be substantially more acceptable than an unconstrained design. Shepherd, Kevin P. and Sullivan, Brenda M. Langley Research Center NASA-TP-3134, L-16913, NAS 1.60:3134 RTOP 537-03-21-03...

A Loudness Calculation Procedure Applied to Shaped Sonic Booms

A Loudness Calculation Procedure Applied to Shaped Sonic Booms PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724999931
Category :
Languages : en
Pages : 32

Book Description
Described here is a procedure that can be used to calculate the loudness of sonic booms. The procedure is applied to a wide range of sonic booms, both classical N-waves and a variety of other shapes of booms. The loudness of N-waves is controlled by overpressure and the associated rise time. The loudness of shaped booms is highly dependent on the characteristics of the initial shock. A comparison of the calculated loudness values indicates that shaped booms may have significantly reduced loudness relative to N-waves having the same peak overpressure. This result implies that a supersonic transport designed to yield minimized sonic booms may be substantially more acceptable than an unconstrained design. Shepherd, Kevin P. and Sullivan, Brenda M. Langley Research Center NASA-TP-3134, L-16913, NAS 1.60:3134 RTOP 537-03-21-03...

A Loudness Calculation Procedure Applied to Shaped Sonic Booms

A Loudness Calculation Procedure Applied to Shaped Sonic Booms PDF Author: Kevin P. Shepherd
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 20

Book Description


A Loudness Calculation Procedure Applied to Shaped Sonic Booms

A Loudness Calculation Procedure Applied to Shaped Sonic Booms PDF Author: Kevin P. Shepherd
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

Book Description


Laboratory Study of Effects of Sonic Boom Shaping on Subjective Loudness and Acceptability

Laboratory Study of Effects of Sonic Boom Shaping on Subjective Loudness and Acceptability PDF Author: Jack D. Leatherwood
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

Book Description


Subjective Response to Simulated Sonic Booms with Ground Reflections

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Publisher:
ISBN:
Category : Aerodynamic noise
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Book Description


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