Download or read book A Time dependent Method for Calculating Supersonic Blunt body Flow Fields with Sharp Corners and Embedded Shock Waves written by Richard W. Barnwell and published by . This book was released on 1970 with total page 76 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 1974 with total page 892 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 Heat transfer and Flow field Tests of the McDonnell Douglas Martin Marietta Space Shuttle Configurations written by Richard K. Matthews and published by . This book was released on 1973 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerothermodynamic tests of Phase B space shuttle configurations proposed by McDonnell Douglas--Martin Marietta were conducted at Mach numbers 8 and 10.5. Test conditions provided both Mach number and Reynolds number simulation for typical ascent and reentry trajectories. This report provides a comprehensive analysis of the major test results and also presents data comparisons with theoretical calculations. Specific areas covered are ascent heating and shock interference, booster reentry heating and flow fields, and orbiter reentry analysis which includes leeside heating, windward shock angles and flow fields, windward surface heating, and boundary-layer transition.
Download or read book Heat transfer and Flow field Tests of the North American Rockwell General Dynamics Convair Space Shuttle Configurations written by W. R. Martindale and published by . This book was released on 1973 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerothermodynamic tests of Phase B space shuttle configurations proposed by North American Rockwell/General Dynamics Convair were conducted at Mach number 8. Test conditions provided both Mach number and Reynolds number simulation for typical ascent and reentry trajectories. This report provides a comprehensive analysis of the major test results and also presents data comparisons with theoretical calculations. Specific areas covered are: ascent heating and shock interference, booster reentry heating and flow fields, and orbiter reentry including leeside heating, windward shock angles and flow fields, windward surface heating, and boundary-layer transition.
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1968 with total page 478 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Bibliography for the Numerical Solution of Partial Differential Equations written by John H. Giese and published by . This book was released on 1969 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt: A list of 2561 references to the numerical solution of partial differential equations has been compiled. References to reviews in several abstracting journals have been given, and a crude index has been prepared. (Author).
Download or read book Flow field Investigation for Large angle Cones with Short Spikes at a Mach Number of 9 6 written by W. Frank Staylor and published by . This book was released on 1970 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Real gas Effects on the Drag and Trajectories of a Nonlifting 140 Conical Aeroshell During Mars Entry written by Dennis O. Allison and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Pressure Distributions on Bluff Tension shell Shapes written by James Wayne Sawyer and published by . This book was released on 1970 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to improve the accuracy in calculating pressure distributions for various tension-shell decelerator shapes and to evaluate the effects on derived shapes resulting from the application of different pressure distributions. Pressure distributions given by Newtonian and integral-relation theory were each used to derive tension-shell shapes. Experimental pressure distributions were obtained from two windtunnel models - one model shape was derived by using a Newtonian pressure distribution and the other shape was derived by using an integral-relation pressure distribution for a Mach number of 3.0 - and were compared with theoretical pressure distributions. The tests were conducted at a Mach number of 3.0, at zero angle of attack, and at a Reynolds number of 10.4 X 106 based on maximum model diameter. Tension-shell shapes were also derived by using the experimental pressure distributions and were compared with both the Newtonianderived shape and the integral-relation-derived shape for a Mach number of 3.0.
Download or read book Space Shuttle Aerothermodynamics Technology Conference Held at Ames Research Center Moffett Field Calif December 15 16 1971 written by and published by . This book was released on 1972 with total page 470 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 1970 with total page 744 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Compilation of Research Reports of Physical Research Division Dynamic Loads Division Loads Division 1921 1973 written by Gloria R. Champine and published by . This book was released on 1977 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distributions on 140 160 and 180 cones at Mach Numbers from 2 30 to 4 63 and Angles of Attack from 0 to 20 written by James Franklin Campbell and published by . This book was released on 1969 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1980 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1968 with total page 814 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1977 with total page 1034 pages. Available in PDF, EPUB and Kindle. Book excerpt:
