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Wind Tunnel Investigation Of Sonic Boom Characteristics Of Two Simple Wing Models At Mach Numbers From 23 To 463
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Book Synopsis Wind-tunnel Investigation of Sonic-boom Characteristics of Two Simple Wing Models at Mach Numbers from 2.3 to 4.63 by : Davis S. Miller
Download or read book Wind-tunnel Investigation of Sonic-boom Characteristics of Two Simple Wing Models at Mach Numbers from 2.3 to 4.63 written by Davis S. Miller and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Sonic-boom Characteristics of Two Simple Wing Models at Mach Numbers from 2.3 to 4.63 by : David S. Miller
Download or read book Wind-tunnel Investigation of Sonic-boom Characteristics of Two Simple Wing Models at Mach Numbers from 2.3 to 4.63 written by David S. Miller and published by . This book was released on 1971 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Investigation at a Mach Number of 2.01 of the Sonic-boom Characteristics of Three Wing-body Combinations Differing in Wing Longitudinal Location by : Odell A. Morris
Download or read book A Wind-tunnel Investigation at a Mach Number of 2.01 of the Sonic-boom Characteristics of Three Wing-body Combinations Differing in Wing Longitudinal Location written by Odell A. Morris and published by . This book was released on 1962 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Sonic-boom Characteristics of a Delta-wing-body Combination at Mach Numbers of 1.41 and 2.01 by : Odell A. Morris
Download or read book Wind-tunnel Investigation of Sonic-boom Characteristics of a Delta-wing-body Combination at Mach Numbers of 1.41 and 2.01 written by Odell A. Morris and published by . This book was released on 1966 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of Some Aspects of the Sonic Boom by Means of Wind-tunnel Measurements of Pressures about Several Bodies at a Mach Number of 2.01 by : Harry W. Carlson
Download or read book An Investigation of Some Aspects of the Sonic Boom by Means of Wind-tunnel Measurements of Pressures about Several Bodies at a Mach Number of 2.01 written by Harry W. Carlson and published by . This book was released on 1959 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Flow-field Development for a Series of Sonic-boom Wind-tunnel Models by :
Download or read book Investigation of Flow-field Development for a Series of Sonic-boom Wind-tunnel Models written by and published by . This book was released on 1971 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Sonic-boom Characteristics in the Extreme Near Field of a Complex Airplane Model at Mach Numbers of 1.5, 1.8, and 2.5 by : Odell A. Morris
Download or read book Sonic-boom Characteristics in the Extreme Near Field of a Complex Airplane Model at Mach Numbers of 1.5, 1.8, and 2.5 written by Odell A. Morris and published by . This book was released on 1970 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Sonic-boom Characteristics of a Delta-wing-body Combination at Mach Numbers of 0.41 and 2.01 by : United States. National Aeronautics and Space Administration
Download or read book Wind-tunnel Investigation of Sonic-boom Characteristics of a Delta-wing-body Combination at Mach Numbers of 0.41 and 2.01 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1966 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Correlation of Sonic-boom Theory with Wind-tunnel and Flight Measurements by : Harry W. Carlson
Download or read book Correlation of Sonic-boom Theory with Wind-tunnel and Flight Measurements written by Harry W. Carlson and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Investigation at a Mach Number of 2.01 of the Sonic-boom Characteristics of Three Wing-body Combinations Differing in Wing Longitudinal Location by : Odell A. Morris
Download or read book A Wind-tunnel Investigation at a Mach Number of 2.01 of the Sonic-boom Characteristics of Three Wing-body Combinations Differing in Wing Longitudinal Location written by Odell A. Morris and published by . This book was released on 1962 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Aircraft Sonic Boom Characteristics from Experimental Near Field Results by : Raymond Morton Hicks
Download or read book Prediction of Aircraft Sonic Boom Characteristics from Experimental Near Field Results written by Raymond Morton Hicks and published by . This book was released on 1967 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : Harry W. Carlson
Download or read book 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 written by Harry W. Carlson and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Investigation of Sonic-boom Pressure Distributions of Bodies of Revolution at Mach 2.96, 3.83, and 4.63 by : Barrett L. Shrout
Download or read book A Wind-tunnel Investigation of Sonic-boom Pressure Distributions of Bodies of Revolution at Mach 2.96, 3.83, and 4.63 written by Barrett L. Shrout and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements of sonic boom pressure distribution of bodies of revolution at Mach 2.96, 3.83, and 4.63 in Unitary Plan wind tunnel.
Book Synopsis Second Conference on Sonic Boom Research by : Ira R. Schwartz
Download or read book Second Conference on Sonic Boom Research written by Ira R. Schwartz and published by . This book was released on 1968 with total page 208 pages. Available in PDF, EPUB and Kindle. Book excerpt: Proceedings of a conference on sonic boom reduction in supersonic transport flight. Topics include shock wave propagation and refraction, prediction methods for acoustic attenuation, and aerodynamic engineering aspects.
Book Synopsis Wind-tunnel Investigation of the Sonic-boom Characteristics of Three Proposed Supersonic Transport Configurations by :
Download or read book Wind-tunnel Investigation of the Sonic-boom Characteristics of Three Proposed Supersonic Transport Configurations written by and published by . This book was released on 1963 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Third Conference on Sonic Boom Research by : Ira R. Schwartz
Download or read book Third Conference on Sonic Boom Research written by Ira R. Schwartz and published by . This book was released on 1971 with total page 474 pages. Available in PDF, EPUB and Kindle. Book excerpt: Prediction methods for sonic boom generation and propagation with overpressure minimization in supersonic transport design and operation.
Book Synopsis Wind-tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1/62-scale Model of the X-1E at Supersonic Speeds by : Arthur Henderson
Download or read book Wind-tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1/62-scale Model of the X-1E at Supersonic Speeds written by Arthur Henderson and published by . This book was released on 1956 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation to determine the static longitudinal and lateral stability characteristics of a 1/62-scale model of the X-1E has been conducted in the Langley 9-inch supersonic tunnel. Tests were made at Mach numbers of 1.62, 1.94, 2.22, 2.40, and 2.62 on the wing-body, wing-body-vertical-tail, and complete model configurations. Detailed analysis of the test results has not been made.