Download or read book Characteristics of Major Active Wind Tunnels at the Langley Research Center written by William T. Schaefer and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains a brief description of each of the major active wind tunnels at the Langley Research Center.
Download or read book Characteristics of Major Active Wind Tunnels at the Langley Research Center written by William T. Schaefer and published by . This book was released on 1965 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Characteristics of Major Active Wind Tunnels at the Langley Research Center written by William T. Schaefer and published by . This book was released on 1965 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains a brief description of each of the major active wind tunnels at the Langley Research Center.
Download or read book Characteristics of Major Active Wind Tunnels at the Langley Research Center written by William T. Jr Schaefer and published by . This book was released on 1965 with total page 52 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 1991 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Cryogenic Wind Tunnels A Comprehensive Annotated Bibliography written by Marie H. Tuttle and published by . This book was released on 1991 with total page 146 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 1977 with total page 836 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 1991 with total page 376 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA s Contributions to Aeronautics Volume 2 Flight Environment NASA SP 2010 570 Vol 2 2010 written by and published by . This book was released on 2011 with total page 1070 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Monthly Catalogue United States Public Documents written by and published by . This book was released on 1965 with total page 1732 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Flow field Development for a Series of Sonic boom Wind tunnel Models written by and published by . This book was released on 1971 with total page 28 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 1978 with total page 802 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 1988 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Cryogenic Wind Tunnels written by Marie H. Tuttle and published by . This book was released on 1985 with total page 76 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 Government wide Index to Federal Research Development Reports written by and published by . This book was released on 1965 with total page 954 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flow Patterns and Pressure Distributions Around a Bluff Afterbody in the Wake of a 120 Cone for Various Separation Distances at Mach 3 0 written by William D. Deveikis and published by . This book was released on 1971 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation of an attached inflatable decelerator concept was conducicd at a Mach number of 3.0 with solid models to observe the effects of varying the separarron distance between the 120 (degrees) cone forebody and the inflated afterbody shape on flow patterns 2nd pressure distributions. Flow-visualization tests were conducted for separation distances cry to 4.74 forebody diameters and at free-stream Reynolds numbers, based on afterbody maximum diameter, between 0.57 X 10 (to the 6 power) and 3.20 X 10 (to the 6 power). Pressure-distribution tests were conducted For separation distances up to 2.49 forebody diameters at free-stream Reynolds numbers, nased on afterbody maximum diameter, between 10.0 X and 11.8 X 10 (to the 6 power). The afterbody was constructed with a burble fence so that the afterbody-to-forebody frontal area ratlo was 6.2.
