Department Of Aeronautics Research Articles

The dynamic scheduling of aircraft in the near terminal area : Roger G. Dear, Department of Quantitative Methods, California State University, Fullerton, CA 92634. (Dissertation in the Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139).

The dynamic scheduling of aircraft in the near terminal area : Roger G. Dear, Department of Quantitative Methods, California State University, Fullerton, CA 92634. (Dissertation in the Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139).

An analytical study of advanced terminal area air traffic management and control : Chen-Chung Hsin, MPW 543, MITRE Corp., Westgate Research Park, McLean VA 22101. (Dissertation at the Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139).

Originally presented as the author's thesis, (Ph. D.) in the M.I.T. Dept. of Aeronautics and Astronautics, 1976

The Impact of High Inflation Rates on the Demand for Air Passenger Transportation. Richard L. Vitek and Nawal K. Taneja. Flight Transportation Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139. May 1975. 117p. $5

The Impact of High Inflation Rates on the Demand for Air Passenger Transportation. Richard L. Vitek and Nawal K. Taneja. Flight Transportation Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139. May 1975. 117p. $5

New Directions for Forecasting Air Travel Passenger Demand. Donald S. Garvett and Nawal K. Tanejo. Flight Transportation Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139. July 1974. 163p plus appendices

New Directions for Forecasting Air Travel Passenger Demand. Donald S. Garvett and Nawal K. Tanejo. Flight Transportation Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139. July 1974. 163p plus appendices

Development of data analysis in sound and vibration

The development of both the philosophy of and the hardware for data analysis in sound and vibration at the I.S.V.R. during the past decade is described, in the context both of earlier progress in the subject in the Department of Aeronautics (as it then was) of the University of Southampton and of the rapid contemporaneous progress in both the mathematical techniques and electronic products for digital computation.

A technique for determining the operational characteristics of a thermoelectric module: H. Y. Wong and W. Shakun, Department of Aeronautics and Fluid Mechanics, University of Glasgow, Glasgow W.2, Scotland. Energy Conversion12, 41–44 (1972)

A technique for determining the operational characteristics of a thermoelectric module: H. Y. Wong and W. Shakun, Department of Aeronautics and Fluid Mechanics, University of Glasgow, Glasgow W.2, Scotland. Energy Conversion12, 41–44 (1972)

A technique for determining the operational characteristics of a thermoelectric module: H. Y. Wong and W. Shakun, Department of Aeronautics and Fluid Mechanics, University of Glasgow, Glasgow W.2, Scotltland. Energy Conversion12, 41–44 (1972)

A technique for determining the operational characteristics of a thermoelectric module: H. Y. Wong and W. Shakun, Department of Aeronautics and Fluid Mechanics, University of Glasgow, Glasgow W.2, Scotltland. Energy Conversion12, 41–44 (1972)

A technique for determining the operational characteristics of a thermoelectric module: H. Y. Wong and W. Shakun, Department of Aeronautics and Fluid Mechanics, University of Glasgow, Glasgow W.2, Scotland. Energy Conversion12, 41–44 (1972)

A technique for determining the operational characteristics of a thermoelectric module: H. Y. Wong and W. Shakun, Department of Aeronautics and Fluid Mechanics, University of Glasgow, Glasgow W.2, Scotland. Energy Conversion12, 41–44 (1972)

Airport Noise Monitoring

This report describes the monitoring requirements of the proposed noise regulations for California airports. The requirements include measuring the noise of each aircraft under the takeoff and approach paths at points which are analogous to those of the Federal Aviation Regulation for aircraft certification. Additionally, they require monitoring of community noise exposure on a contour of equal community noise equivalent level, which is analogous to a contour constructed in accordance with federal noise exposure forecast methods. The paper also discusses the rationale of the quantities to be monitored and their relationship to quantities used by the federal government for certification and land use planning. [This work was supported by the Department of Aeronautics of the State of California.]

Angular Distribution of Thermal Radiation from a Cylindrical Particle Cloud

Received December 3, 1970; presented as Paper 71-78 at the AIAA 9th Aerospace Sciences Meeting, New York, January 2527, 1971; synoptic received June 7, 1971. Full paper is available from AIAA. Price: AIAA members, $1.50; nonmembers, $2.00. Microfiche, $1.00. Order must be accompanied by remittance. Index category: Radiation and Radiative Heat Transfer. * Major, Department of Aeronautics. f Cadet First Class, Department of Aeronautics. .2 is .05. Emission from Surface r = 2 h/d=5 . —._ Isotropic Scattering ----Anisotropic Scattering

Compressible Turbulent Boundary-Layer Heat Transfer to Rough Surfaces

Progress in Aeronautical Sciences, Vol. 7, edited by Kuchemann et al., Pergamon Press, New York, 1966. 14 Squire, H. B., Analysis of the Vortex-Breakdown Phenomenon, Part I, Rept. 102, 1960, Aeronautics Department, Imperial College, London. 16 Benjamin, T. B., of the Breakdown Phenomenon, Journal of Fluid Mechanics, Vol. 14, Pt. 4, Dec. 1962, p. 593. 16 Benjamin, T. B., Significance of the Breakdown Phenomenon, Transactions of the American Society of Mechanical Engineers, Journal of Basic Engineering, Vol. 87, No. 2, 1965, pp. 518, 1091. 17 Benjamin, T. B., Some Developments in the Theory of Breakdown, Journal of Fluid Mechanics^ Vol. 28, Pt. 1, April 1967, p. 65. 18 Ludwieg, H., Zur Erklarung der Instabilitat der iiber angestellten Deltaniigeln auftreten freien Wirkbelkerne, Zeitschriftfiir Flugwissenschaften, Vol. 10, 1962, p. 242. 19 Ludwieg, H., Experimented Nachprufung der Stabilitatstheorien fur reibungsfreie Stromungen mit schraubenformigen Stromlinien, Zeitschrift fur Flugwissenschaften, Vol. 12, 1964, p. 304. 20 Jones, J. P., Breakdown of Vortices in Separated Rept. 140, 1960, University of Southampton Aeronautics and Astronautics Department. 21 Hall, M. G., On the Occurrence and Identification of Breakdown, TN 66283, 1966, Royal Aircraft Establishment, Farnborough Hants. 22 Bossel, H. H., Vortex Breakdown Flowfield, The Physics of Vol. 12, No. 3, 1969, p. 498. 23 Leibovich, S., Weakly Non-Linear Waves in Rotating Fluids, Journal of Fluid Mechanics, Vol. 42, Pt. 4, Dec. 1970, p. 803. 24 Pedley, T. J., On the Instability of Viscous Flow in a Rapidly Rotating Pipe, Journal of Fluid Mechanics, Vol. 35, Pt. 1, Jan. 1969, p. 97. 25 Talbot, L., Laminar Swirling Pipe Journal of Applied Mechanics, Vol. 21, No. 1, March 1954, p. 1. 26 Joseph, D. D. and Munson, B. R., Global Stability of Spiral Journal of Fluid Mechanics, Vol. 43, Pt. 3, Sept. 1970, p. 545. 27 Henderson, F. M., Open Channel Flow, Macmillan, New York, 1966, pp. 45, 215^218.

Analysis of optimum charged particle size based on the conversion efficiency of electrogasdynamic generators : Oscar Biblarz, Naval Postgraduate School, Monterey, California. Asst. Prof., Department of Aeronautics. Energy Conversion10, 207–213 (1970)

Analysis of optimum charged particle size based on the conversion efficiency of electrogasdynamic generators : Oscar Biblarz, Naval Postgraduate School, Monterey, California. Asst. Prof., Department of Aeronautics. Energy Conversion10, 207–213 (1970)

Analysis of optimum charged particle size based on the conversion efficiency of electrogasdynamic generators : Oscar Biblarz, Naval Postgraduate School, Monterey, California, Asst. Prof., Department of Aeronautics. Energy Conversion10, 207–213 (1970)

Analysis of optimum charged particle size based on the conversion efficiency of electrogasdynamic generators : Oscar Biblarz, Naval Postgraduate School, Monterey, California, Asst. Prof., Department of Aeronautics. Energy Conversion10, 207–213 (1970)

Analysis of optimum charged particle size based on the conversion efficiency of electrogasdynamic generators : Oscar Biblarz, Naval Postgraduate School, Monterey, California, Asst. Prof., Department of Aeronautics. Energy Conversion10, 207–213 (1970)

Analysis of optimum charged particle size based on the conversion efficiency of electrogasdynamic generators : Oscar Biblarz, Naval Postgraduate School, Monterey, California, Asst. Prof., Department of Aeronautics. Energy Conversion10, 207–213 (1970)

Personalities in the news

The first Fellow has been appointed under the terms of a trust, set up at Imperial College, London, in memory of the late Mr Donald Campbell, for the advancement of all forms of research in the field of aerodynamics. He is Mr I. P. Castro, who will work in the Department of Aeronautics at Imperial College.

Twenty-Second British Commonwealth Lecture

The Twenty-Second British Commonwealth Lecture, “Aeronautical Research in India”, was given by Dr. S. Dhawan, MA, BSc(Eng), MS, FRAeS, Director of the Indian Institute of Science, Bangalore, on 3rd November 1966. The Chair was taken by the President, Mr. A. D. Baxter, MEng, FRAeS, and the distinguished audience included His Excellency Dr. J. Mehta, High Commissioner for India.Before the Lecture the President introduced Lord Caldecote, DSC, MA, FRAeS, immediate Past President of the Society of British Aerospace Companies Limited, who presented the four SB AC Scholarship Awards for 1966 to the recipients.Introducing the Lecturer, Mr. Baxter said that the British Commonwealth Lecture had been established immediately after the Second World War to foster interest and understanding in aeronautical developments between Great Britain and her partners in the Commonwealth. He thought that object had been successfully achieved by the efforts of a long and distinguished list of lecturers, both from home and overseas; now they were to add another distinguished name to that list. Dr. Dhawan had taken his first degree in mathematics and physics at Lahore in 1938; in 1941 he obtained his MA from the Punjab University and, from the same university, his BSc in Engineering in 1944. After a period as an Assistant Supervisor with the Hindustan Aircraft Company, he was selected by the Government of India for advanced studies abroad in aeronautics. Dr. Dhawan had gone to the United States where he took a Masters Degree in Aeronautics at the University of Minnesota and a PhD in Aeronautics at the Californian Institute of Technology. Returning to India in 1951, he joined the Department of Aeronautics at the Indian Institute of Science, becoming Assistant Professor in 1952 and Professor and Head of the Department in 1955 and, since 1963 Director of the Institute.

STRAIN MEASUREMENTS BY METHOD OF PRE‐TENSIONING

StrainVolume 3, Issue 1 p. 14-14 STRAIN MEASUREMENTS BY METHOD OF PRE-TENSIONING H. Y. WONG, H. Y. WONG Department of Aeronautics and Fluid Mechanics The University of GlasgowSearch for more papers by this authorF. H. KELLING, F. H. KELLING Department of Aeronautics and Fluid Mechanics The University of GlasgowSearch for more papers by this author H. Y. WONG, H. Y. WONG Department of Aeronautics and Fluid Mechanics The University of GlasgowSearch for more papers by this authorF. H. KELLING, F. H. KELLING Department of Aeronautics and Fluid Mechanics The University of GlasgowSearch for more papers by this author First published: January 1967 https://doi.org/10.1111/j.1475-1305.1967.tb00860.xAboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onFacebookTwitterLinkedInRedditWechat No abstract is available for this article. Volume3, Issue1January 1967Pages 14-14 RelatedInformation

Integral Axi-Symmetric Nozzle Design

SummaryThis is an extension of the design method described in ref. 1 to the compressible flow in integral nozzles comprising both subsonic (contraction) and supersonic (effusor) parts. The nozzles are axially symmetric and will be considered as isentropic convertors of low speed high enthalpy inviscid gas to a high speed, relatively low enthalpy state, heat transfer effects being ignored. The key advantage of the method over existing hybrid design methods(2'3'4'5) is that no assumption is made as to conditions in the “sonic” throat region before expansion in the effusor, the design being integral from low speed inlet to high speed outlet. A slight disadvantage of the method is that of ref 1, namely that a nozzle of an ideally infinite extent has to be truncated both at inlet and outlet. However, for a given nozzle length this limitation can be biased towards the relatively insensitive low subsonic inlet to benefit correspondingly outlet conditions to the extent that it should be possible to make the maximum variation from the mean in the cross-sectional speed at outlet less than 0.01 per cent. The method is being applied to design integral hypersonic nozzle units for the projected small intermittent hypersonic facility in the Department of Aeronautics and Space Technology. This tunnel will have a nominal working-section diameter of 2 in and the flow will be accelerated from low speed (about 20 ft/sec) at inlet to Mach numbers of either 5, 6, or 7 at outlet to the working section using three alternative nozzles.

Effect of Preharvest Desiccation on Grain Sorghum1

Crop ScienceVolume 5, Issue 6 cropsci1965.0011183X000500060012x p. 523-526 Article Effect of Preharvest Desiccation on Grain Sorghum1 R. W. Bovey, Search for more papers by this authorM. K. McCarty, Former Instructor in Agronomy (presently Research Agronomist, Crops Research Division, ARS, USDA, Department of Range and Forestry, Texas A&M University, College Station, Texas) and Research Agronomist, Crops Research Division, ARS, USDA, Department of Agronomy, University of Nebraska, Lincoln.Search for more papers by this author R. W. Bovey, Search for more papers by this authorM. K. McCarty, Former Instructor in Agronomy (presently Research Agronomist, Crops Research Division, ARS, USDA, Department of Range and Forestry, Texas A&M University, College Station, Texas) and Research Agronomist, Crops Research Division, ARS, USDA, Department of Agronomy, University of Nebraska, Lincoln.Search for more papers by this author First published: 01 November 1965 https://doi.org/10.2135/cropsci1965.0011183X000500060012xCitations: 4 1 Published with the approval of the Director as Paper No. 1691, Journal Series, Nebraska Agricultural Experiment Station. This research was supported in part by the Nebraska State Department of Aeronautics. A portion of a thesis submitted by the senior author in partial fulfillment of the requirements for the Ph.D. degree, Department of Agronomy, Unversity of Nebraska. AboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onEmailFacebookTwitterLinked InRedditWechat Citing Literature Volume5, Issue6November–December 1965Pages 523-526 RelatedInformation

Bending of Circular Plates Sealing an Incompressible Liquid

Technical Briefs Bending of Circular Plates Sealing an Incompressible Liquid A. D. Kerr A. D. Kerr Department of Aeronautics and Astronautics, New York University, New York, N. Y.; Cold Regions Research and Engineering Laboratory (CRREL), U. S. Army Search for other works by this author on: This Site PubMed Google Scholar Author and Article Information A. D. Kerr Department of Aeronautics and Astronautics, New York University, New York, N. Y.; Cold Regions Research and Engineering Laboratory (CRREL), U. S. Army J. Appl. Mech. Sep 1965, 32(3): 704-706 (3 pages) https://doi.org/10.1115/1.3627288 Published Online: September 1, 1965 Article history Received: April 24, 1964 Revised: March 3, 1965 Online: September 15, 2011