Aeropulsive Characteristics At Mach Numbers Up To 22 Of Axisymmetric And Nonaxisymmetric Nozzles Installed On An F 18 Model

Author : Francis J. Capone
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.62/5 ( download)

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Download or read book Aeropulsive Characteristics at Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model written by Francis J. Capone and published by . This book was released on 1982 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation to determine the aeropropulsive characteristics of nonaxisymmetric nozzles on an F-18 jet effects model was conducted in the Langley 16-foot transonic tunnel and the AEDC 16-foot supersonic wind tunnel. The performance of a two dimensional convergent-divergent nozzle, a single expansion ramp nozzle, and a wedge nozzle was compared with that of the baseline axisymmetric nozzle. Test data were obtained at static conditions and at Mach numbers from 0.60 to 2.20 at an angle of attack of 0 deg. Nozzle pressure ratio was varied from jet-off to about 20.

Author : George T. Carson
Publisher :
ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.66/5 ( download)

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Download or read book Aeropropulsive Characteristics of Nonaxisymmetric-nozzle Thrust Reversers at Mach Numbers from 0 to 1.20 written by George T. Carson and published by . This book was released on 1984 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Edward J. Ray
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.98/5 ( download)

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Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : James F. Campbell
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.26/5 ( download)

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Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Donald P. Hearth
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.86/5 ( download)

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Download or read book Investigation at Supersonic and Subsonic Mach Numbers of Auxiliary Inlets Supplying Secondary Air Flow to Ejector Exhaust Nozzles written by Donald P. Hearth and published by . This book was released on 1956 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results indicated increases in auxiliary-inlet pressure recovery with increases in scoop height relative to the boundary-layer thickness. The pressure recovery increased at about the same rate as theoretically predicted for an inlet in a boundary layer having a one-seventh power profile, but was only about 0.68 to 0.75 of the theoretically obtainable values. Under some operating conditions, flow from the primary jet was exhausted through the auxiliary inlet. This phenomenon could be predicted from the ejector pumping characteristics.

Author : Eleanor Costilow Guentert
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.62/5 ( download)

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Download or read book Design of Axisymmetric Exhaust Nozzles by Method of Characteristics Incorporating a Variable Isentropic Exponent written by Eleanor Costilow Guentert and published by . This book was released on 1959 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Francis J. Capone
Publisher :
ISBN 13 :
Total Pages : 280 pages
Book Rating : 4.28/5 ( download)

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Download or read book Parametric Investigation of Single-expansion-ramp Nozzles at Mach Numbers from 0.60 to 1.20 written by Francis J. Capone and published by . This book was released on 1992 with total page 280 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Dennis E. Fuller
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.04/5 ( download)

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Download or read book Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63 written by Dennis E. Fuller and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Owen H. Davis
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.64/5 ( download)

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Download or read book Performance of a Mach Number 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range 1.97 to 0.79 written by Owen H. Davis and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Eugene N. Brooks
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.11/5 ( download)

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Download or read book Static Aerodynamic Characteristics of a Model of a Typical Subsonic Jet-transport Airplane at Mach Numbers from 0.40 to 1.20 written by Eugene N. Brooks and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: