Download or read book Jet Effects on the Drag of Conical Afterbodies for Mach Numbers of 0 6 to 1 28 written by James M. Jr Cubbage and published by . This book was released on 1957 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Jet Effects on the Drag of Conical Afterbodies at Spersonic Speeds written by William B. Compton and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Jet Effects on Base Pressures of Conical Afterbodies at Mach 1 91 and 3 12 written by L. Eugene Baughman and published by . This book was released on 1957 with total page 111 pages. Available in PDF, EPUB and Kindle. Book excerpt: Data are presented which show the effect of a jet on base pressure for a series of conical afterbody-jet-nozzle combinations having boattail angles that varied from o to 11 degrees and base-to-jet diameter ratios that varied from 1.11 to 2.67. The jet nozzles had exit angles from 0 to 20 degrees and were designed for exit Mach numbers from 1.0 to 3.2. Pressure ratios up to 30 tested for both a cold (air) and a hot (rocket) jet. The investigation was conducted at free-stream Mach numbers of 1.91 to 3.12.
Download or read book The Aerothermodynamics of Aircraft Gas Turbine Engines written by and published by . This book was released on 1978 with total page 770 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Convergent Ejector Nozzles on the Boattail Drag of a 16 Conical Afterbody at Mach Number of 0 6 to 1 26 written by James M. Cubbage and published by . This book was released on 1958 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Mass Injection and Jet Flow Simulation Effects on Transonic Afterbody Drag written by Wladimiro Calarese and published by . This book was released on 1978 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation has been performed to determine the effects of boattail injection and jet flow simulation on the afterbody drag of a slender body of revolution in the transonic regime at zero angle of attack, such as engine nacelles and boattailed afterbodies with isolated engines. A correlation between sting and jet diameter has been established. The jet plume and the nozzle pressure ratio simulators have been found appropriate and useful as a testing technique. Boattail mass injection usually produces a drag coefficient reduction and is more effective at high nozzle pressure ratios. Boattail injection is more effective if used in regions of separated flow. (Author).
Download or read book Index of NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Afterbody Ejection Configurations on the Performance at Transonic Speeds of a Pylon supported Nacelle Model Having a Hot jet Exhaust written by John M. Swihart and published by . This book was released on 1962 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect on Base Drag of Recessing the Bases of Conical Afterbodies at Subsonic and Transonic Speeds written by William B. Compton and published by . This book was released on 1968 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1989 with total page 72 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 A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1960 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book U S Government Research Reports written by and published by . This book was released on 1963 with total page 1028 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1979 with total page 1074 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamics Interference written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel and published by . This book was released on 1971 with total page 512 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 1156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
