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Filed under: Fuel tanks- Rear end structural crashworthiness of unitized construction vehicles, design development and design verification. Final report. (1973), by Robert L. Anderson and E. Enserink (page images at HathiTrust)
- Rear end structural crashworthiness of unitized construction vehicles - summary report. Final report. (1973), by Robert L. Anderson and E. Enserink (page images at HathiTrust)
- Study of post-crash factors in automobile collisions. Volume 1. Final report. (1975), by J. A. Austin, F. R. Wagner, A. Hogan, and G. Bryner (page images at HathiTrust)
- Development of a school bus fuel system integrity compliance procedure. Final report. (1975), by G. W. Morrow and N. Johnson (page images at HathiTrust)
- Study of post-crash factors in automobile collisions. Volume 2. Final report. (1975), by J. A. Austin, F. R. Wagner, A. Hogan, and G. Bryner (page images at HathiTrust)
- Spilled fuel ignition sources and countermeasures. Final report. (1975), by N. Johnson and S. Sanderson (page images at HathiTrust)
- Evaluation methodology for federal motor vehicle safety standards. Volume I: executive summary. Final report. (1977), by R. L. Braun, R. H. Cronin, N. A. David, A. V. Fend, and J. R. Norman (page images at HathiTrust)
- Evaluation methodology for federal motor vehicle safety standards. Volume II: technical findings. Final report. (1977), by R. L. Braun, R. H. Cronin, N. A. David, A. V. Fend, and J. R. Norman (page images at HathiTrust)
- Review of four federal motor vehicle safety standards: FMVSS 214, 215, 301, 208. Task #1 report. (1977), by Hans C. Joksch and Joseph C. Reidy (page images at HathiTrust)
- Final design and implementation plan for evaluating the effectiveness of FMVSS 301: fuel system integrity. Tasks #4 & #5 report. (1977) (page images at HathiTrust)
- Multidisciplinary accident investigation - school bus locomotive-caboose collision, Lafayette, Oregon, September 8, 1976. MDAI team report. (1977), by Eugene E. Flamboe and J. Ouelett (page images at HathiTrust)
- Automobile fuel tanks. (1979), by Lois Flynn (page images at HathiTrust)
- Cost evaluation for nine Federal Motor Vehicle Safety Standards: Task VIII - FMVSS 301, fuel system integrity - determination of the model year when manufacturers made changes to meet Standard's 1976 requirements. Final report. (1979), by R. F. McLean and G. Lisiecki (page images at HathiTrust)
- A statistical evaluation of the effectiveness of the 1976 version of FMVSS 301: Fuel System Integrity. Final report. (1982), by Donald W. Reinfurt (page images at HathiTrust)
- Investigation of transport airplane fuselage fuel tank installations under crash conditions. Final report. (1989), by G. Wittlin (page images at HathiTrust)
- An analysis of fires in passenger cars, light trucks, and vans. (1994), by J. Tessner (page images at HathiTrust)
- A 1992 Dodge Ram B250 van rear impact CNG fuel tank integrity. Final report. (1993), by K. W. Looker (page images at HathiTrust)
- Final report of a 1991 Plymouth Acclaim rear impact CNG fuel tank integrity. (1994), by C. A. Markusic (page images at HathiTrust)
- Boating accident investigations 1973 ; fire and explosion (Tampa, Fla., 1974), by Underwriters' Laboratories, Robert Loeser, and United States Coast Guard (page images at HathiTrust)
- Vibration characteristics of a cylinder partially filled with liquid with an attached elastic drain pipe (National Aeronautics and Space Administration ;, 1970), by Robert J. Kroll, Langley Research Center, and University of Cincinnati (page images at HathiTrust)
- Fuel dump tanks for HRT (United States Atomic Energy Commission, Technical Information Service ;, 1955), by Sidney Visner, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
- HRT entrainment separator design study (U.S. Atomic Energy Commission, Technical Information Service, 1954), by C. L. Segaser, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
- Photographic investigation of liquid behavior on temperature and liquid-vapor sensors used in low-gravity environment (National Aeronautics and Space Administration ;, 1967), by James A. Berns, Ralph C. Nussle, Frederick C. Yeh, and Lewis Research Center (page images at HathiTrust)
- Design optimization of natural laminar flow bodies in compressible flow (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), by Simha S. Dodbele, Langley Research Center, and Inc ViGYAN (page images at HathiTrust)
Filed under: Airplanes -- Fuel tanks- Investigation of mechanisms of potential aircraft fuel tank vent fires and explosions caused by atmospheric electricity (National Aeronautics and Space Administration :, 1964), by United States. Federal Aviation Agency, United States National Aeronautics and Space Administration, and Lockheed-California Company (page images at HathiTrust)
- Analytical heat transfer investigation of insulated liquid methane wing tanks for supersonic cruise aircraft (National Aeronautics and Space Administration :, 1970), by Eugene J. Pleban, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Comparative study of fuselage tanks for liquid-methane-fueled supersonic aircraft (National Aeronautics and Space Administration, 1968), by Rene E. Chambellan, William A. Bevevino, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- The control of carbon dioxide cryodeposits (National Aeronautics and Space Administration ;, 1973), by Ellsworth L. Sharpe and Langley Research Center (page images at HathiTrust)
- Investigation of minimum corona type currents for ignition of aircraft fuel vapors (National Aeronautics and Space Administration, 1960), by M. M. Newman, J. D. Robb, and Lightning and Transients Research Institute (page images at HathiTrust)
- Moment of inertia and damping of fluid in tanks undergoing pitching oscillations (National Advisory Committee for Aeronautics, 1953), by Edward Widmayer, James R. Reese, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick tapered, unswept wing (National Advisory Committee for Aeronautics, 1954), by Roland D. English, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Flutter investigation of a true-speed dynamic model with various tip-tank configurations (National Advisory Committee for Aeronautics, 1955), by John L. Sewall, William B. Igoe, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model (National Advisory Committee for Aeronautics, 1956), by Albert P. Martina, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A theoretical analysis of the effects of fuel motion on airplane dynamics (National Advisory Committee for Aeronautics, 1951), by Albert A. Schy and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Some effects of fluid in pylon-mounted tanks on flutter (National Advisory Committee for Aeronautics, 1955), by James R. Reese and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- A Review of the flammability hazard of jet A fuel vapor in civil transport aircraft fuel tanks (Federal Aviation Administration, Office of Aviation Research ;, 1998), by Richard Hill and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
- Aircraft wing fuel tank environmental simulator tests for evaluation of antimisting fuels (Federal Aviation Administration Technical Center ;, 1984), by P. M. McConnell, H. K. Mehta, F. F. Tolle, Boeing Military Airplane Company, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
- A practical external cardiac pacemaker-defibrillator (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1956), by Terence F. McGuire, Donald A. Rosenbaum, Stanley C. White, United States. Air Force. Air Research and Development Command, Aero Medical Laboratory, and Wright Air Development Center (page images at HathiTrust)
Filed under: Liquid propellant rockets -- Fuel tanks- Effect of contact angle and tank geometry on the configuration of the liquid-vapor interface during weightlessness (National Aeronautics and Space Administration, 1963), by Donald A. Petrash, Edward W. Otto, Ralph C. Nussle, and Lewis Research Center (page images at HathiTrust)
- NASA TN D-3746 (National Aeronautics and Space Administration :, 1966), by Joseph D. Derdul, Donald A. Petrash, Lynn S. Grubb, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-5387 (National Aeronautics and Space Administration ;, 1969), by Robert J. Stochl, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Filed under: Rockets (Aeronautics) -- Fuel tanks- The dynamic behavior of liquids in moving containers, with applications to space vehicle technology. (Scientific and Technical Information Division, National Aeronautics and Space Administration; for sale by Supt. of Docs., U. S. Govt. Print. Off., 1966), by H. Norman Abramson and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Effect of throttling on interface behavior and liquid residuals in weightlessness (National Aeronautics and Space Administration ;, 1974), by Eugene P. Symons and Lewis Research Center (page images at HathiTrust)
- Abort separation study of a shuttle orbiter and external tank at hypersonic speeds (National Aeronautics and Space Administration ;, 1975), by Peter T. Bernot and Langley Research Center (page images at HathiTrust)
- Single launch lunar habitat derived from NSTS external tank (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Charles B. King and Langley Research Center (page images at HathiTrust)
- Fabrication of an internally insulated filament wound liquid hydrogen propellant tank (National Aeronautics and Space Administration, 1964), by C. B. Shriver, Goodyear Aerospace Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- An experimental investigation of the viscous damping of liquid sloshing in spherical tanks (National Aeronautics and Space Administration, 1963), by Irving E. Sumner, Andrew J. Stofan, and Lewis Research Center (page images at HathiTrust)
- NASA TN D-3746 (National Aeronautics and Space Administration :, 1966), by Joseph D. Derdul, Donald A. Petrash, Lynn S. Grubb, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Low-density foam for insulating liquid-hydrogen tanks (National Aeronautics and Space Administration ;, 1969), by Irving E. Sumner, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- NASA TN D-5258 (National Aeronautics and Space Administration ;, 1969), by Donald C. Urasek, Robert E. Connelly, Phillip R. Meng, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-5291 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Ronald G. Huff, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Design, fabrication, and structural testing of a lightweight shadow shield for deep-space application (National Aeronautics and Space Administration ;, 1977), by David Miao, Richard L. DeWitt, James R. Barber, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- An experimental evaluation of metallic diaphragms for positive fuel expulsion in the Atmosphere Explorer hydrazine propulsion subsystem (National Aeronautics and Space Administration ;, 1973), by William L. Woodruff and Goddard Space Flight Center (page images at HathiTrust)
- Ring-baffle pressure distribution and slosh damping in large cylindrical tanks (National Aeronautics and Space Administration ;, 1972), by Harland F. Scholl, Phillip K. Davis, David G. Stephens, and Langley Research Center (page images at HathiTrust)
- Basic performance of a multilayer insulation system containing 20 to 160 layers (National Aeronautics and Space Administration ;, 1974), by Robert J. Stochl and Lewis Research Center (page images at HathiTrust)
- Analytic and experimental evaluation of shadow shields and their support members for thermal control of space vehicles (National Aeronautics and Space Administration ;, 1974), by Robert J. Boyle, Robert J. Stochl, and Lewis Research Center (page images at HathiTrust)
- Pressurant requirements for discharge of liquid methane from a 1.52-meter- (5-ft- ) diameter spherical tank under both static and slosh conditions (National Aeronautics and Space Administration ;, 1974), by Richard L. DeWitt, Thomas O. McIntire, and Lewis Research Center (page images at HathiTrust)
- Computer programs for pressurization (ramp) and pressurized expulsion from a cryogenic liquid propellant tank (National Aeronautics and Space Administration ;, 1974), by Philip A. Masters and Lewis Research Center (page images at HathiTrust)
- Low-gravity reorientation in a scale-model Centaur liquid-hydrogen tank (National Aeronautics and Space Administration ;, 1973), by Jack A. Salzman, Raymond F. Lacovic, William J. Masica, and Lewis Research Center (page images at HathiTrust)
- Effects of some external-store mounting arrangements and store shapes on the buffet and drag characteristics of wingless rocket-powered models at Mach numbers from 0.7 to 1.4 (National Advisory Committee for Aeronautics, 1954), by Homer P. Mason, Allen B. Henning, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
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