Newtonian Aerodynamics For Circular Cones Modified To Procedure Lift At Zero Angle Of Attack
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Author | : Barbara J. Short |
Publisher | : |
Total Pages | : 42 |
Release | : 1969 |
Genre | : Angle of attack (Aerodynamics) |
ISBN | : |
Download Newtonian Aerodynamics for Circular Cones Modified to Produce Lift at Zero Angle of Attack Book in PDF, Epub and Kindle
Author | : Barbara J. Short |
Publisher | : |
Total Pages | : 31 |
Release | : 1969 |
Genre | : |
ISBN | : |
Download Newtonian Aerodynamics for Circular Cones Modified to Procedure Lift at Zero Angle of Attack Book in PDF, Epub and Kindle
Author | : Barbara J. Short |
Publisher | : |
Total Pages | : 0 |
Release | : 1969 |
Genre | : Angle of attack (Aerodynamics) |
ISBN | : |
Download Newtonian Aerodynamics for Circular Cones Modified to Produce Lift at Zero Angle of Attack Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 314 |
Release | : 1969 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, Epub and Kindle
Author | : JIM A. PENLAND |
Publisher | : |
Total Pages | : 1 |
Release | : 1961 |
Genre | : |
ISBN | : |
Download Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 130 Degrees Book in PDF, Epub and Kindle
Force tests of a series of right circular cones having semivertex angles ranging from 5 to 45 degrees and a series of right circular cone-cylinder configurations having semivertex angles ranging from 5 to 20 degrees and an afterbody fineness ratio of 6 have been made in the Langley 11inch hypersonic tunnel at a Mach number of 6.83, a Reynolds number of 0.24 x 10 to the 6th power per inch, and angles of attack up to 130 degrees. An analysis of the results made use of the Newtonian and modified Newtonian theories and the exact theory. A comparison of the experimental data of both cone and cone-cylinder configurations with theoretical calculations shows that the Newtonian concept gives excellent predictions of trends of the force characteristics and the locations with respect to angle of attack of the points of maximum lift, maximum drag, and maximum lift-drag ratio. Both the Newtonian and exact theories give excellent predictions of the sign and value of the initial lift-curve slope. (Author).
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 966 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
Download NASA Scientific and Technical Reports Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 756 |
Release | : 1983 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, Epub and Kindle
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.
Author | : Julius E. Harris |
Publisher | : |
Total Pages | : 28 |
Release | : 1967 |
Genre | : Noses (Space vehicles) |
ISBN | : |
Download Aerodynamic Characteristics of a Spherically Blunted 25° Cone at a Mach Number of 20 Book in PDF, Epub and Kindle
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 956 |
Release | : 1970 |
Genre | : Science |
ISBN | : |
Download NASA Scientific and Technical Reports and Publications for 1969 - A Selected Listing Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : |
Release | : 1969 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, Epub and Kindle