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Thermal Design For Areas Of Interference Heating On Actively Cooled Hypersonic Aircraft
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Book Synopsis Thermal Design for Areas of Interference Heating on Actively Cooled Hypersonic Aircraft by : R. L. Herring
Download or read book Thermal Design for Areas of Interference Heating on Actively Cooled Hypersonic Aircraft written by R. L. Herring and published by . This book was released on 1978 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Review of Convectively Cooled Structures for Hypersonic Flight by :
Download or read book Review of Convectively Cooled Structures for Hypersonic Flight written by and published by . This book was released on 1986 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Current Technology for Thermal Protection Systems by :
Download or read book Current Technology for Thermal Protection Systems written by and published by . This book was released on 1992 with total page 336 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summarizes the history and operational experience of thermal protection systems utilized in the national space program, and also covers development efforts in thermal insulation, refractory materials and coatings, actively cooled structures, and two-phase thermal control systems.
Download or read book NASA Conference Publication written by and published by . This book was released on 1992 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Actively Cooled Plate Fin Sandwich Structural Panels for Hypersonic Aircraft by : L. M. Smith
Download or read book Actively Cooled Plate Fin Sandwich Structural Panels for Hypersonic Aircraft written by L. M. Smith and published by . This book was released on 1979 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt: An unshielded actively cooled structural panel was designed for application to a hypersonic aircraft. The design was an all aluminum stringer-stiffened platefin sandwich structure which used a 60/40 mixture of ethylene glycol/water as the coolant. Eight small test specimens of the basic platefin sandwich concept and three fatigue specimens from critical areas of the panel design was fabricated and tested (at room temperature). A test panel representative of all features of the panel design was fabricated and tested to determine the combined thermal/mechanical performance and structural integrity of the system. The overall findings are that; (1) the stringer-stiffened platefin sandwich actively cooling concept results in a low mass design that is an excellent contender for application to a hypersonic vehicle, and (2) the fabrication processes are state of the art but new or modified facilities are required to support full scale panel fabrication.
Book Synopsis Flightweight Radiantly and Actively Cooled Panel by : Charles P. Shore
Download or read book Flightweight Radiantly and Actively Cooled Panel written by Charles P. Shore and published by . This book was released on 1982 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design and Fabrication of a Radiative Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft by : D. A. Ellis
Download or read book Design and Fabrication of a Radiative Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft written by D. A. Ellis and published by . This book was released on 1978 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design and Fabrication of a Stringer Stiffened Discrete Tube Actively Cooled Panel for a Hypersonic Aircraft by : Frank M. Anthony
Download or read book Design and Fabrication of a Stringer Stiffened Discrete Tube Actively Cooled Panel for a Hypersonic Aircraft written by Frank M. Anthony and published by . This book was released on 1981 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High Heat Flux Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft by : Leland C. Koch
Download or read book High Heat Flux Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft written by Leland C. Koch and published by . This book was released on 1978 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 500 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalogue, United States Public Documents by :
Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1980 with total page 1268 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1968 with total page 1256 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1976 with total page 1194 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Internal Convective Cooling Systems for Hypersonic Aircraft by : F. M. Anthony
Download or read book Internal Convective Cooling Systems for Hypersonic Aircraft written by F. M. Anthony and published by . This book was released on 1975 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Parametric studies were conducted to investigate the relative merits of construction materials, coolants, and cooled panel concepts for internal convective cooling systems applied to airframe structures of hydrogen-fueled hypersonic aircraft. These parametric studies were then used as a means of comparing various cooled structural arrangements for a hypersonic transport and a hypersonic research airplane. The cooled airplane studies emphasized weight aspects as related to the choice of materials, structural arrangements, structural temperatures, and matching of the cooling system heat load to the available hydrogen fuel-flow heat sink. Consideration was given to reliability and to fatigue and fracture aspects, as well. Even when auxiliary thermal protection system items such as heat shielding, insulation, and excess hydrogen for cooling are considered the more attractive actively cooled airframe concepts indicated potential payload increases of from 40 percent to over 100 percent for the hypersonic transport as compared to the results of previous studies of the same vehicle configuration with an uncooled airframe.
Book Synopsis A Fuselage/tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles: Active Cooling System Analysis by :
Download or read book A Fuselage/tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles: Active Cooling System Analysis written by and published by . This book was released on 1975 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Recent Advances in Structures for Hypersonic Flight, Part 1 by :
Download or read book Recent Advances in Structures for Hypersonic Flight, Part 1 written by and published by . This book was released on 1978 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA SP. written by and published by . This book was released on 1993 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt: