An Investigation Of The Influence Of Lift On Sonic Boom Intensity By Means Of Wind Tunnel Measurements Of The Pressure Fields Of Several Wing Body Combinations At A Mach Number Of 201 PDF Download

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An Investigation of the Influence of Lift on Sonic-boom Intensity by Means of Wind-tunnel Measurements of the Pressure Fields of Several Wing-body Combinations at a Mach Number of 2.01

An Investigation of the Influence of Lift on Sonic-boom Intensity by Means of Wind-tunnel Measurements of the Pressure Fields of Several Wing-body Combinations at a Mach Number of 2.01
Author: Harry W. Carlson
Publisher:
Total Pages: 44
Release: 1961
Genre: Aerodynamic load
ISBN:

Download An Investigation of the Influence of Lift on Sonic-boom Intensity by Means of Wind-tunnel Measurements of the Pressure Fields of Several Wing-body Combinations at a Mach Number of 2.01 Book in PDF, ePub and Kindle


An Investigation of the Influence of Lift on Sonic-Boom Intensity by Means of Wind-Tunnel Measurements of the Pressure Fields of Several Wing-Body Combinations at a Mach Number of 2.01

An Investigation of the Influence of Lift on Sonic-Boom Intensity by Means of Wind-Tunnel Measurements of the Pressure Fields of Several Wing-Body Combinations at a Mach Number of 2.01
Author: Harry W. Carlson
Publisher:
Total Pages: 1
Release: 1961
Genre:
ISBN:

Download An Investigation of the Influence of Lift on Sonic-Boom Intensity by Means of Wind-Tunnel Measurements of the Pressure Fields of Several Wing-Body Combinations at a Mach Number of 2.01 Book in PDF, ePub and Kindle

An investigation of the effect of lift on sonicboom intensity was performed by means of windtunnel measurements of the pressure fields surrounding small wing-body combinations. Effects of lift were found to be real and significant. Measured bow-shock intensities agreed fairly well with, but were consistently less than, shock intensities estimated by theoretical methods. Available flight data were examined for correlation with wind-tunnel test results. (Author).


Ground Measurements of Sonic-boom Pressures for the Altitude Range of 10,000 to 75,000 Feet

Ground Measurements of Sonic-boom Pressures for the Altitude Range of 10,000 to 75,000 Feet
Author: Harvey H. Hubbard
Publisher:
Total Pages: 56
Release: 1964
Genre: Sonic boom
ISBN:

Download Ground Measurements of Sonic-boom Pressures for the Altitude Range of 10,000 to 75,000 Feet Book in PDF, ePub and Kindle

The U.S. Air Force, National Aeronautics and Space Administration, and Federal Aviation Agency have engaged in a joint research program for the purpose of measuring sonic-boom pressure signatures. These measurements are presented for several locations for flight tests of fighter and bomber airplanes in the altitude range from about 10,000 to 75,000 feet and at Mach numbers from 1.1 to 2.0. Data were obtained for a variety of atmospheric wind and temperature gradients and for various flight paths and acceleration rates.


NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 410
Release: 1963
Genre:
ISBN:

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NASA Technical Report

NASA Technical Report
Author:
Publisher:
Total Pages: 540
Release: 1964
Genre: Aerodynamics
ISBN:

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