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The Influence Of Design Pressure Ratio And Divergence Angle On The Thrust Of Convergent Divergent Propelling Nozzles
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Book Synopsis The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles by : Aeronautical Research Council
Download or read book The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles written by Aeronautical Research Council and published by . This book was released on 1957 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles by : P. F. Ashwood
Download or read book The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles written by P. F. Ashwood and published by . This book was released on 1957 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles by : P. F. Ashwood
Download or read book The Influence of Design Pressure Ratio and Divergence Angle on the Thrust of Convergent-divergent Propelling Nozzles written by P. F. Ashwood and published by . This book was released on 1955 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1962 with total page 898 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of Several Conical Convergent-divergent Rocket-type Exhaust Nozzles by : C. E. Campbell
Download or read book Performance of Several Conical Convergent-divergent Rocket-type Exhaust Nozzles written by C. E. Campbell and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to obtain nozzle performance data with relatively large-scale models at pressure ratios as high as 120. Conical convergent-divergent nozzles with divergence angles alpha of 15, 25, and 29 deg. were each tested at area ratios of approximately 10, 25, and 40. Heated air (1200 F) was supplied at the nozzle inlet at pressures up to 145 pounds per square inch absolute and was exhausted into quiescent air at pressures as low as 1.2 pounds per square inch absolute. Thrust ratios for all nozzle configurations are presented over the range of pressure ratios attainable and were extrapolated when possible to design pressure ratio and beyond. Design thrust ratios decreased with increasing nozzle divergence angle according to the trend predicted by the (1 + cos alpha)/2 parameter. Decreasing the nozzle divergence angle resulted in sizable increases in thrust ratio for a given surface-area ratio (nozzle weight), particularly at low nozzle pressure ratios. Correlations of the nozzle static pressure at separation and of the average static pressure downstream of separation with various nozzle parameters permitted the calculation of thrust in the separated-flow region from unseparated static-pressure distributions. Thrust ratios calculated by this method agreed with measured values within about 1 percent.
Book Synopsis Internal Performance of Several Divergent-shroud Ejector Nozzles with High Divergence Angles by : Arthur M. Trout
Download or read book Internal Performance of Several Divergent-shroud Ejector Nozzles with High Divergence Angles written by Arthur M. Trout and published by . This book was released on 1957 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Study of Effects of Geometric Variables on Performance of Conical Rocket - Engine Exhaust Nozzles by : Harry E. Bloomer
Download or read book Experimental Study of Effects of Geometric Variables on Performance of Conical Rocket - Engine Exhaust Nozzles written by Harry E. Bloomer and published by . This book was released on 1961 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Study of Effects of Geometric Variables on Performance of Contoured Rocket Engine Exhaust Nozzles by : Harry E. Bloomer
Download or read book Experimental Study of Effects of Geometric Variables on Performance of Contoured Rocket Engine Exhaust Nozzles written by Harry E. Bloomer and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Nozzle Inlet Geometry on Performance of a Swiveled Convergent-divergent Nozzle by : Albert J. Pavli
Download or read book Effect of Nozzle Inlet Geometry on Performance of a Swiveled Convergent-divergent Nozzle written by Albert J. Pavli and published by . This book was released on 1959 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Influence of Pressure Ratio and Divergence Angle on the Shock Position in Two Dimensional Over-expaned, Convergent-divergent Nozzles by : Aeronautical Research Council
Download or read book The Influence of Pressure Ratio and Divergence Angle on the Shock Position in Two Dimensional Over-expaned, Convergent-divergent Nozzles written by Aeronautical Research Council and published by . This book was released on 1957 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions by : Mary L. Mason
Download or read book The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions written by Mary L. Mason and published by . This book was released on 1980 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Investigation of Off-design Performance of Divergent-ejector-type Rocket Nozzles by : Laurence W. Gertsma
Download or read book Preliminary Investigation of Off-design Performance of Divergent-ejector-type Rocket Nozzles written by Laurence W. Gertsma and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions by : Mary L. Mason
Download or read book The Effect of Throat Contouring on Two-dimensional Converging-diverging Nozzles at Static Conditions written by Mary L. Mason and published by . This book was released on 1980 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Influence of Pressure Ratio and Divergence Angle on the Shock Position in Two Dimensional, Over-expanded, Convergent-divergent Nozzles by : Peter F. Ashwood
Download or read book The Influence of Pressure Ratio and Divergence Angle on the Shock Position in Two Dimensional, Over-expanded, Convergent-divergent Nozzles written by Peter F. Ashwood and published by . This book was released on 1956 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Approximate Theoretical Method for Modeling the Static Thrust Performance of Non-axisymmetric Two-dimensional Convergent-divergent Nozzles by :
Download or read book An Approximate Theoretical Method for Modeling the Static Thrust Performance of Non-axisymmetric Two-dimensional Convergent-divergent Nozzles written by and published by . This book was released on 1995 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Research Abstracts and Reclassification Notice by : United States. National Advisory Committee for Aeronautics
Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1956 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Internal Performance Including Thrust Vectoring and Reversing of Tow-dimensional Convergent-divergent Nozzles by : Richard J. Re
Download or read book Static Internal Performance Including Thrust Vectoring and Reversing of Tow-dimensional Convergent-divergent Nozzles written by Richard J. Re and published by . This book was released on 1984 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
