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Author :
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (317 download)
Download or read book In-flight and Simulated Aircraft Fuel Temperature Measurements written by and published by . This book was released on 1990 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 568 pages
Book Rating : 4.:/5 (3 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : COORDINATING RESEARCH COUNCIL INC ATLANTA GA.
Publisher :
ISBN 13 :
Total Pages : 65 pages
Book Rating : 4.:/5 (227 download)
Download or read book Low Temperature Behavior of Fuels in Simulated Aircraft Tanks written by COORDINATING RESEARCH COUNCIL INC ATLANTA GA. and published by . This book was released on 1983 with total page 65 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lockheed and Boeing each made a series of tests in aircraft fuel tank simulators to provide an improved understanding of the flowability and pumpability of jet fuels at or below their freezing point where waxy components separate. Each simulator represented a section of an aircraft wing fuel tank. Tests simulated the low temperature cruise environment associated with long duration flights under extreme, high-altitude conditions. Holdup, the fraction of unavailable fuel remaining in the tank after attempted fuel withdrawal, was used to characterize pumpability after low temperature exposure. The test fuels were derived from widely differing crude sources and were selected to cover a range of freezing points. Two of the test fuels were common to the Boeing and Lockheed investigations in order to assess variability due to simulator construction. One fuel in the Lockheed program contained a flow improver additive. In the Boeing program, one fuel was a blend of JP-5 and 9% marine diesel fuel. (Author).
Author : Coordinating Research Council. Aviation Fuel, Lubricant, and Equipment Research Committee
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (19 download)
Download or read book Low Temperature Behavior of Fuels in Simulated Aircraft Tanks written by Coordinating Research Council. Aviation Fuel, Lubricant, and Equipment Research Committee and published by . This book was released on 1983 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Perry W. Kirklin
Publisher : ASTM International
ISBN 13 : 0803114311
Total Pages : 165 pages
Book Rating : 4.8/5 (31 download)
Download or read book Aviation Fuel written by Perry W. Kirklin and published by ASTM International. This book was released on 1992 with total page 165 pages. Available in PDF, EPUB and Kindle. Book excerpt: For technical readers in the aviation and fuel industries, and in testing laboratories, explores the history and philosophy of the thermal stability of aviation fuel, and considerations during the fuel's manufacture, storage and transport, use, and assessment. The 13 papers, representing a number of
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Publisher :
ISBN 13 :
Total Pages : 654 pages
Book Rating : 4.:/5 (319 download)
Download or read book NASA SP. written by and published by . This book was released on 1992 with total page 654 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : P. M. McConnell
Publisher :
ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (1 download)
Download or read book Aircraft Wing Fuel Tank Environmental Simulator Tests for Evaluation of Antimisting Fuels written by P. M. McConnell and published by . This book was released on 1984 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: The low temperature performance of antimisting kerosene (AMK) in airframe fuel systems and in certain fuel system components was studied and compared to Jet A fuel. Water vapor ingested into fuel tanks during simulation of repeated descents through clouds and rain had little effect on AMK. AMK retained antimisting properties during exposure to severe environmental flight simulations. Jet pump and boost pump operation had no discernable effect on AMK flammability. Jet pump performance with AMK was adversely affected. Main fuel boost pumps required up to 18 percent more power with AMK that with Jet A, and suction feed performance was lower with ambient and -20 deg C, but better than Jet A and -40 deg C. Boost pump performance was not affected by gel formations produced at low temperatures by the vapor removal return flow shearing of AMK. Aerodynamic heating and cooling of AMK in the fuel tank was similar to Jet A.A high pressure pump and needle valve used to degrade the AMK was inadequate, resulting in filter bypass at low temperatures. (Author).
Author :
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ISBN 13 :
Total Pages : 538 pages
Book Rating : 4.3/5 (91 download)
Download or read book Aeronautical Engineering written by and published by . This book was released on 1991 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Research Council
Publisher : National Academies Press
ISBN 13 : 0309058333
Total Pages : 158 pages
Book Rating : 4.3/5 (9 download)
Download or read book Aviation Fuels with Improved Fire Safety written by National Research Council and published by National Academies Press. This book was released on 1997-09-18 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt: The reduction of the fire hazard of fuel is critical to improving survivability in impact-survivable aircraft accidents. Despite current fire prevention and mitigation approaches, fuel flammability can overwhelm post-crash fire scenarios. The Workshop on Aviation Fuels with Improved Fire Safety was held November 19-20, 1996 to review the current state of development, technological needs, and promising technology for the future development of aviation fuels that are most resistant to ignition during a crash. This book contains a summary of workshop discussions and 11 presented papers in the areas of fuel and additive technologies, aircraft fuel system requirements, and the characterization of fuel fires.
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ISBN 13 :
Total Pages : 1638 pages
Book Rating : 4.:/5 (31 download)
Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1995 with total page 1638 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ira P. Jones
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.3/5 (91 download)
Download or read book Measurements of Aerodynamic Heating Obtained During Demonstration Flight Tests of the Douglas D-558-II Airplane written by Ira P. Jones and published by . This book was released on 1952 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Royce P. Bradley
Publisher :
ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.:/5 (227 download)
Download or read book High Temperature Hydrocarbon Fuels Research in an Advanced Aircraft Fuel System Simulator on Fuel AFFB-14-70 written by Royce P. Bradley and published by . This book was released on 1974 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hydrocarbon fuels tend to form deposits in the thermal environment associated with high mach number flight. The Advanced Aircraft Fuel System Simulator provides thermal stability data on fuels which are used to determine aircraft fuel system design criteria, operational limits of fuels, and to aid in the development of small-scale thermal stability test devices. Fuel AFFB-14-70, the seventh fuel in a series, was tested under cyclic and steady-state conditions. Steady-state manifold tests were run to determine the effect of dissolved oxygen on thermal stability. The results of tests using manifold tubes with widely different surface finishes are reported. (Modified author abstract).
Author : Coordinating Research Council, Inc. Aviation Fuel, Lubricant, and Equipment Research Committee
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (618 download)
Download or read book Low Temperature Behaviour of Fuels in Simulated Aircraft Tanks written by Coordinating Research Council, Inc. Aviation Fuel, Lubricant, and Equipment Research Committee and published by . This book was released on 1983 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Richard D. Banner
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.3/5 (91 download)
Download or read book Flight Measurements of Airplane Structural Temperatures at Supersonic Speeds written by Richard D. Banner and published by . This book was released on 1957 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Skin and structural temperatures have been obtained on the X-1B and X-1E research airplanes under transient aerodynamic heating conditions at speeds up to Mach numbers near 2.0. Extensive temperature measurements were obtained throughout the X-1B airplane, and temperature distributions are shown on the nose cone, the wing, and the vertical tail. Temperatures for the X-1E wing leading edge and internal wing structure were compared with similar data for the X-1B. No critical skin and structural temperatures were obtained on the two airplanes over the range of these tests. Simplified calculations of the skin temperatures in the laminar-flow regions of the nose cone and the leading edges agreed favorably with the general trends in the measured data. The flat-plate skin-temperature calculations in the turbulent-flow regions agreed favorably with the measured data on the nose cone and at the midsemispan station of the wing but overestimated the vertical-tail skin temperatures and also the upper wing skin temperature near the wing tip. The relatively low values of the upper skin temperatures that were measured at the wing tip were believed to be caused by separated-flow effects in this region.
Author : Roger A. Fields
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (31 download)
Download or read book A Study of the Accuracy of a Flight-heating Simulation and Its Effect on Load Measurement written by Roger A. Fields and published by . This book was released on 1970 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Harold Goodman
Publisher :
ISBN 13 :
Total Pages : 129 pages
Book Rating : 4.:/5 (227 download)
Download or read book High Temperature Hydrocarbon Fuels Research in an Advanced Aircraft Fuel System Simulator on Fuel AFFB-11-68 written by Harold Goodman and published by . This book was released on 1969 with total page 129 pages. Available in PDF, EPUB and Kindle. Book excerpt: At elevated temperatures, hydrocarbon jet fuels tend to form deposits which decrease heat exchanger efficiency and plug screens and filter elements. In order to quantify this tendency so that it may be predicted, it is necessary to obtain comparative test results on a simulated aircraft fuel system and small-scale test devices. (Author).
Author : Harold Goodman
Publisher :
ISBN 13 :
Total Pages : 157 pages
Book Rating : 4.:/5 (227 download)
Download or read book High Temperature Hydrocarbon Fuels Research in an Advanced Aircraft Fuel System Simulator on Fuel Affb-9-67 written by Harold Goodman and published by . This book was released on 1968 with total page 157 pages. Available in PDF, EPUB and Kindle. Book excerpt: At elevated temperatures, hydrocarbon jet fuels tend to form deposits which decrease heat exchanger efficiency and plug screens and filter elements. In order to quantify this tendency so that it may be predicted, it is necessary to obtain comparative test results on a simulated aircraft fuel system and small-scale test devices. In the report, the thermal stability of the second fuel (AFFB-9-67) tested in the Advanced Aircraft Fuel System Simulator is quantified in terms of the amount of deposit formed. The quantification of deposit formation is determined under cyclic conditions (mission profiles) and two types of steady state test conditions (steady state and steady state-varied flow). The difference between the two steady state tests is that the steady state test was performed at constant flow rate and heat input and the steady state-varied flow test contained intervals wherein a higher flow rate and no heat input were imposed. In addition to testing in the Simulator, fuel AFFB-9-67 was tested in the standard, gas, research, modified, and micro cokers; as well as other facilities. (Author).
