Analysis of a Jet in a Subsonic Crosswind

Analysis of a Jet in a Subsonic Crosswind
Title Analysis of a Jet in a Subsonic Crosswind PDF eBook
Author
Publisher
Pages 260
Release 1969
Genre Aerodynamics
ISBN

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Title Scientific and Technical Aerospace Reports PDF eBook
Author
Publisher
Pages 662
Release 1982
Genre Aeronautics
ISBN

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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.

Analytic Methods in Aircraft Aerodynamics

Analytic Methods in Aircraft Aerodynamics
Title Analytic Methods in Aircraft Aerodynamics PDF eBook
Author
Publisher
Pages 758
Release 1970
Genre Aerodynamics
ISBN

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Analysis of the Injection of a Heated Turbulent Jet Into a Cross Flow

Analysis of the Injection of a Heated Turbulent Jet Into a Cross Flow
Title Analysis of the Injection of a Heated Turbulent Jet Into a Cross Flow PDF eBook
Author James Franklin Campbell
Publisher
Pages 70
Release 1973
Genre Jets
ISBN

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An investigation has been undertaken to develop a theoretical model of the incompressible jet injection process. The discharge of a turbulent jet into a cross flow was mathematically modeled by using an integral method which accounts for natural fluid mechanisms such as turbulence, entrainment, buoyancy, and heat transfer. The analytical results are supported by experimental data and demonstrate the usefulness of the theory for estimating the trajectory and flow properties of the jet for a variety of injection conditions. The capability of predicting jet flow properties, as well as two- and three- dimensional jet paths, was enhanced by obtaining the jet cross-sectional area during the solution of the conservation equations (a number of previous studies assume a specific growth for the area). Realistic estimates of temperature in the jet fluid were acquired by accounting for heat losses in the jet flow due to forced convection and to entrainment of free-stream fluid into the jet.

NASA Technical Note

NASA Technical Note
Title NASA Technical Note PDF eBook
Author
Publisher
Pages 606
Release 1975
Genre
ISBN

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Applied Mechanics Reviews

Applied Mechanics Reviews
Title Applied Mechanics Reviews PDF eBook
Author
Publisher
Pages 776
Release 1971
Genre Mechanics, Applied
ISBN

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Recent Advances in Aerodynamics

Recent Advances in Aerodynamics
Title Recent Advances in Aerodynamics PDF eBook
Author Anjaneyulu Krothapalli
Publisher Springer Science & Business Media
Pages 752
Release 2012-12-06
Genre Science
ISBN 1461249724

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The Joint Institute for Aeronautics and Acoustics at Stanford University was established in October 1973 to provide an academic environment for long-term cooperative research between Stanford and NASA Ames Research Center. Since its establishment, the In stitute has wnducted theoretical and experimental work in the areas of aerodynamics, acoustics, fluid mechanics, flight dynamics, guid ance and control, and human factors. This research has involved Stanford faculty, research associates, graduate students, and many distinguished visitors in collaborative efforts with the research staff of NASA Ames Research Center. The occasion of the Institute's tenth anniversary was used to reflect back on where that research has brought us, and to consider where our endeavors should be directed next. Thus, an International Symposium was held to review recent advances in the fields relevant to the activities of the Institute and to discuss the areas of research to be undertaken in the future. This anniversary was also chosen a.."1 an opportunity to honor one of the Institute's founders and its di rector, Professor Krishnamurty Karamcheti. It has been his creative inspiration that has provided the ideal research environment at the Joint Institute. The International Symposium on Recent Advances in Aero dynamics and Aconstics was held at Stanford University, Stanford, California, U.S.A., August 22-26, 198:~. Thirty-five distinguished scientists were invited to present a comprehensive review on the fol lowing subject areas: unsteady aerodynamics, jets and shear layers, V /STOL aircraft aerodynamics, rotor dynamics and aerodynamics,.