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Book Slot Jet Interaction Studies of an Ogive Cylinder at M infinity

Download or read book Slot Jet Interaction Studies of an Ogive Cylinder at M infinity written by Ralph Edward Phinney and published by . This book was released on 1968 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental study of the control forces and moments generated by a slot-type secondary jet located near the base of an ogive cylinder in a Mach 4 and 5 free stream was conducted in the NOL Supersonic Tunnel No. 2. The free-stream Reynolds number, based on body length, was held constant at 22,000,000 and the missile angle of attack was varied from -10 to +10 degrees. The jet slot spanned one quadrant of the cylindrical surface and was contained between two low aspect ratio fins. (Author).

Book NASA Technical Note

    Book Details:
  • Author :
  • Publisher :
  • Release : 1967
  • ISBN :
  • Pages : 316 pages

Download or read book NASA Technical Note written by and published by . This book was released on 1967 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1972 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1964 with total page 1148 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Critical Review of Analytical Methods for Estimating Control Forces Produced by Secondary Injection

Download or read book A Critical Review of Analytical Methods for Estimating Control Forces Produced by Secondary Injection written by Michael J Werle and published by . This book was released on 1968 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem discussed is that of theoretically predicting the normal force induced in the boundary layer separation region immediately ahead of a secondary injection port. Attention was limited to the two-dimensional problem of sonic or supersonic normal injection into supersonic or hypersonic mainstreams. A critical review of available experimental studies was conducted in order to isolate those data best representing a two-dimensional state. The resulting compilation of experimental results was thereafter employed as a basis of comparison for available theoretical and empirical flow models. As a result it was found that analytical means are only capable of rough quantitative estimates of control jet effectiveness and that a more detailed flow model is needed to further explain observed phenomenon. The basic features of such a model are formulated and its conceptual validity demonstrated through comparison with experimental results. Problem areas requiring further research are also discussed in detail. (Author).

Book Proceedings of the Fluid Amplification Symposium Sponsored by the Harry Diamond Laboratories 26  27  and 28 October 1965  Vol  IV

Download or read book Proceedings of the Fluid Amplification Symposium Sponsored by the Harry Diamond Laboratories 26 27 and 28 October 1965 Vol IV written by United States. Ordnance Corps (Army) and published by . This book was released on 1965 with total page 312 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Proceedings

Download or read book Proceedings written by and published by . This book was released on 1965 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Proceedings of the Fluid Amplification Symposium

Download or read book Proceedings of the Fluid Amplification Symposium written by and published by . This book was released on 1965 with total page 314 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Interference Induced by Reaction Controls

Download or read book Aerodynamic Interference Induced by Reaction Controls written by F. W. Spaid and published by . This book was released on 1973 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Investigation of Secondary Jets from Two dimensional Nozzles with Various Exit Mach Numbers for Hypersonic Control Application

Download or read book Experimental Investigation of Secondary Jets from Two dimensional Nozzles with Various Exit Mach Numbers for Hypersonic Control Application written by and published by . This book was released on 1967 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book AGARD Conference Proceedings

    Book Details:
  • Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
  • Publisher :
  • Release : 1966
  • ISBN :
  • Pages : 522 pages

Download or read book AGARD Conference Proceedings written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1966 with total page 522 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Separated Flows

Download or read book Separated Flows written by Jean J. Ginoux and published by . This book was released on 1966 with total page 510 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Tactical Missile Aerodynamics

    Book Details:
  • Author : Michael J. Hemsch
  • Publisher : AIAA (American Institute of Aeronautics & Astronautics)
  • Release : 1992
  • ISBN :
  • Pages : 774 pages

Download or read book Tactical Missile Aerodynamics written by Michael J. Hemsch and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1992 with total page 774 pages. Available in PDF, EPUB and Kindle. Book excerpt: This two-volume set includes discussions of the physics of the fluid mechanics phenomena associated with tactical missile flight and the full range of prediction methods required to analyze current and future missiles. It's a valuable resource for missile aerodynamicists, designers, and researchers.