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:
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:
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:
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:
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:
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:
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:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1983 with total page 688 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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:
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:
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:
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:
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.
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:
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.
Download or read book Wind tunnel Investigation of the Validity of a Sonic boom minimization Concept written by Robert J. Mack and published by . This book was released on 1979 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Measurements of Sonic Boom Signatures Using a Continuous Data Acquisition Technique written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-22 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel investigation was conducted in the Langley Unitary Plan Wind Tunnel to determine the effectiveness of a technique to measure aircraft sonic boom signatures using a single conical survey probe while continuously moving the model past the probe. Sonic boom signatures were obtained using both move-pause and continuous data acquisition methods for comparison. The test was conducted using a generic business jet model at a constant angle of attack and a single model-to-survey-probe separation distance. The sonic boom signatures were obtained at a Mach number of 2.0 and a unit Reynolds number of 2 million per foot. The test results showed that it is possible to obtain sonic boom signatures while continuously moving the model and that the time required to acquire the signature is at least 10 times faster than the move-pause method. Data plots are presented with a discussion of the results. No tabulated data or flow visualization photographs are included. Wilcox, Floyd J. and Elmiligui, Alaa A. Langley Research Center SONIC BOOMS; DATA ACQUISITION; WIND TUNNEL TESTS; MACH NUMBER; REYNOLDS NUMBER; INFORMATION FLOW; ANGLE OF ATTACK; WIND TUNNELS
