Download or read book Two dimensional Converging diverging Rippled Nozzles at Transonic Speeds written by John R. Carlson and published by . This book was released on 1994 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Annular Internal external expansion Rocket Nozzles for Large Booster Applications written by James F. Connors and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerial Applicators Spray Nozzle Handbook written by Ivan W. Kirk and published by U.S. Government Printing Office. This book was released on 2004 with total page 248 pages. Available in PDF, EPUB and Kindle. Book excerpt: "The objective of this handbook is to present aerial spray nozzle animation models in tabular format for use as a reference manual at the mix and load station, in the field, or at other locations where computer access is impractical or unavailable."--P. 8.

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:

Download or read book Effect of Geometric Parameters on the Static Performance of an Annular Nozzle with a Concave Central Base written by Charles E. Mercer and published by . This book was released on 1962 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of F 16 Nozzle afterbody Forces at Transonic Mach Numbers with Emphasis on Support System Interference written by Earl A. Price (Jr.) and published by . This book was released on 1979 with total page 416 pages. Available in PDF, EPUB and Kindle. Book excerpt: A comprehensive experimental program was conducted to provide nozzle-afterbody data with a minimum interference support system on a 1/9-scale F-16 model and to determine the interference induced on the afterbody-nozzle region by a sting, a wingtip, and a strut model support system. The investigation was conducted over the Mach number range from 0.6 to 1.5 and at angles of attack from 0 to 9 deg. Interference was evaluated by comparison of nozzle-afterboy axial and normal forces obtained from integrating pressure data. The results include parametric studies of the efects of various components of the wingtip support system (i.e., the support blade axial position, wingtip boom diameter, boom spacing, and boom-tip axial location). High-pressure air at ambient temperature was utilized for exhaust plume simulation. The results indicate that a sting support passing through the nozzle with the jet effects simulated by an annular jet appears to offer a minimum interference support system for the type of nozzle-afterbody test described in this report.

Download or read book Static Performance of a Cruciform Nozzle with Multiaxis Thrust vectoring and Reverse thrust Capabilities written by David J. Wing and published by . This book was released on 1992 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Jet Velocity and Axial Location of Nozzle Exit on the Performance of a Twin jet Afterbody Model at Mach Numbers Up to 2 2 written by Bobbly Lee Berrier and published by . This book was released on 1969 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Air film Cooling of a Supersonic Nozzle written by Bing H. Lieu and published by . This book was released on 1964 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental study was made of the internal air-film cooling of a Mach 2.4, nonadiabatic wall, axially symmetric nozzle. The main stream air was heated to supply temperatures from 672 to 1212 R at supply pressures from 115 to 465 psia. The film coolant air was injected through a single peripheral slot at an angle of 10 degrees from the nozzle wall. The coolant-to-main stream mass flow ratios were varied up to 20%. Steady-state nozzle wall temperatures were measured in both the subsonic and the supersonic flow regimes. The turbulent pipe flow equation of Dittus and Boelter was found to be applicable in predicting the heat transfer rates in the absence of film cooling. A modified version of the semi-empirical equation of Hatch and Papell was found applicable in estimating the filmcooled nozzle wall temperatures. (Author).

Download or read book Afterbody Drag Investigation of a Twin nozzle Fighter type Model at Mach Numbers from 0 6 to 1 5 written by Earl A. Price (Jr.) and published by . This book was released on 1972 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Measured Base Pressures on Several Twin Rocket nozzle Configurations at Mach Nubmers of 0 6 to 1 4 with Effects Due to Nozzle Canting and Stabilizing Fins written by James M. Cubbage and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Differential Pressures on a Pitot venturi and a Pitot static Nozzle Over 360 pitch and Yaw written by Elliott G. Reid and published by . This book was released on 1927 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Supersonic Investigation of Nozzle Hinge Moments of a Modified Saturn C 1 Model with and Without Jet Flow written by Nickolai Charczenko and published by . This book was released on 1963 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Design Criteria for the Spacing of Nozzles and Reinforced Openings in Cylindrical Nuclear Pressure Vessels and Pipe written by Samuel Eli Moore and published by . This book was released on 1982 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Turbulence Studies of a Rectangular Slotted Noise suppressor Nozzle written by James C. Laurence and published by . This book was released on 1960 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Comparison of Simplex and Dual orifice Fuel Nozzles with Ambient and Heated Fuel in an Annular Turbojet Combustor written by Donald F. Schultz and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A full-scale annular combustor was operated with simplex fuel nozzles of three flow ranges and with dual-orifice fuel nozzles. The dual-orifice nozzles provided combustion efficiencies within 2 to 3 percent of the peak values obtained with any of the simplex atomizers. A wide range of operating conditions including altitude relight, simulated takeoff, Mach 2.7 cruise, and Mach 3.0 cruise were studied. Measurements were made of combustion efficiency, pattern factor , flame radiation, smoke emission, and response to rapid increase in fuel flow. Fuel heated to 300 [degree] F (423 K) was used in many of the tests; heated fuel usually increased combustion efficiency.

Download or read book Effect of Fuels and Fuel nozzle Characteristics on Performance of an Annular Combustor at Simulated Altitude Conditions written by RIchard J. McCafferty and published by . This book was released on 1948 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: