Research Catalog

  • The characteristics of fatigue damage in the fuselage riveted lap splice joint [microform] / Robert S. Piascik ; Scott A. Willard.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1997]
    • 1997
  • Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panel [microform] / R. Keith Bird and Dennis L. Dicus.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment [microform] / Mark S. Chaffin and John D. Berry.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Cabin fuselage structural design with engine installation and control system [microform].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Cabin-fuselage-wing structural design concept with engine installation [microform].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Advanced composites structural concepts and materials technologies for primary aircraft structures [microform] : structural response and failure analysis / W.J. Dorris ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992
  • Advanced composites structural concepts and materials technologies for primary aircraft structures [microform] : design-manufacturing concept assessment / Robert L. Chu ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992
  • Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages [microform] / Venkit Iyer.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1990.
    • 1990
  • Application of a design-build-team approach to low cost and weight composite fuselage structure [microform] / L.B. Ilcewicz ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991
  • Fuselage shell and cavity response measurements on a DC-9 test section [microform] / M.A. Simpson ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
  • A review of ice accretion data from a model rotor icing test and comparison with theory [microform] / Randall K. Britton.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
  • A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas [microform] / Robert J. Mack, Kathy E. Needleman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1990.
    • 1990
  • Aircraft interior noise reduction by alternate resonance tuning [microform] : progress report for the period ending December, 1988 / prepared by Donald B. Bliss ... [et al.].

    • Text
    • Durham, N.C. : Dept. of Mechanical Engineering and Materials Science, Duke University ; [Washington, D.C.? : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Center, distributor, 1989]
    • 1989
  • The characterization of widespread fatigue damage in fuselage structure [microform] / Robert S. Piascik, Scott A. Willard, Matthew Miller.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Numerical simulation of helicopter engine plume in forward flight [microform] : final report cooperative agreement #NCC2-5061 / Arsenio C.B. Dimanlig, Cornelis P. van Dam, Earl P.N. Duque.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models [microform] / P.N. Bansal ... [et al.].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985
  • Helicopter tail rotor noise analyses [microform] : final technical report ; period, June 1, 1985 - January 31, 1986 / Albert R. George and S.-T. Chou.

    • Text
    • Ithaca, New York : Sibley School of Mechanical and Aerospace Engineering, Cornell University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers [microform] / John C. Wilson and Henry L. Kelley.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, distributor], 1986.
    • 1986
  • Load transfer in the stiffener-to-skin joints of a pressurized fuselage [microform] : NASA grant NAG-1-537, performance period, November 1, 1991 to April 30, 1995 / Eric R. Johnson, Naveen Rastogi.

    • Text
    • Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, 1995]
    • 1995
  • Development of stitched/RTM primary structures for transport aircraft [microform] / Arthur V. Hawley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • Novel composites for wing and fuselage applications [microform] / L.H. Sobel, C. Buttitta, and J.A. Suarez.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • A record of all marker bands found in the upper rivet rows of 2 adjacent bays from a fuselage lap splice joint [microform] / Scott A. Willard.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Compression response of a sandwich fuselage keel panel with and without damage [microform] / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Novel composites for wing and fuselage applications [microform] : textile reinforced composites and design guidelines / J.A. Suarez ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Analytical studies of boundary layer generated aircraft interior noise [microform] / M.S. Howe and P.L. Shah.

    • Text
    • Boston, MA : Boston University, College of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Novel composites for wing and fuselage applications. Task 1. Novel wing design concepts [microform] / J.A. Suarez ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension [microform] / Marshall Rouse ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure [microform] / C.E. Harris ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Rotor-fuselage interactions [microform] / John D. Berry, Nicolas Bettschart.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Methodology for predicting the onset of widespread fatigue damage in lap-splice joints [microform] / J.C. Newman, Jr. ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Vibro-acoustics modal testing at NASA Langley Research Center [microform] / Richard S. Pappa, Jocelyn I. Pritchard, Ralph D. Buehrle.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Analysis and design of fuselage structures including residual strength prediction methodology [microform] : final report for NASA grant NAG-1-1588 / by the Department of Aerospace Engineering, College of Engineering and Technology, Old Dominion University ; principal investigator, Norman F. Knight, Jr.

    • Text
    • [Norfolk, Va.] : Old Dominion University Research Foundation ; [Washington, DC National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Crashworthy evaluation of a 1/5-scale model composite fuselage concept [microform] / Karen E. Jackson and Edwin L. Fasanella.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads [microform] / James H. Starnes, Jr. ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Design of fuselage shapes for natural laminar flow [microform] / S. S. Dodbele and C. P. van Dam, P. M. H. W. Vijgen.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986
  • Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell [microform] / Naveen Rastogi and Eric R. Johnson.

    • Text
    • Blacksburg, Va. : Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60750
  • Asymptotic modal analysis and statistical energy analysis [microform] / Earl H. Dowell and Linda F. Peretti.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfieldl, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS63966
  • Fuselage design for a specified Mach-sliced area distribution [microform] / Raymond L. Barger and Mary S. Adams.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68306
  • An evaluation of the pressure proof test concept for thin sheet 2024-T3 [microform] / D.S. Dawicke ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67255
  • NASA airframe structural integrity program [microform] / Charles E. Harris.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67254
  • Experimental measurement of structural power flow on an aircraft fuselage [microform] : progress report no. 6, Jan.-June 1989 / J.M. Cuschieri.

    • Text
    • Boca Rotan, Fla. : Florida Atlantic University, College of Engineering, Dept. of Ocean Engineering, Center for Acoustics and Vibrations ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67727
  • Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes [microform] / James S. Bowman, Jr., Randy S. Hultberg, Colin A. Martin.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68623
  • Failure mechanisms of laminates transversely loaded by bolt push-through [microform] / William Allen Waters, Jr. and Jerry G. Williams.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/gPO/LPS85281
  • Unsteady transonic flow calculations for wing-fuselage configurations [microform] / John T. Batina.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
  • A study of the utilization of advanced composites in fuselage structures of commercial aircraft [microform] : final report / D. J. Watts, ... [et al.].

    • Text
    • Long Beach, Calif. : Douglas Aircraft Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88416
  • Light aircraft sound transmission study [microform] / sponsored by NASA ; submitted by Mahabir Atwal ... [et al.].

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, [Langley Research Center, 1983]
    • 1983
  • Flow field survey near the rotational plane of an advanced design propeller on a Jetstar airplane [microform] / Kevin Robert Walsh.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985.
    • 1985
  • Vertical drop test of a transport fuselage center section including the wheel wells [microform] / M. Susan Williams and Robert J. Hayduk.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS95200
  • Field-incidence transmission of treated orthotropic and laminated composite panels [microform] / Leslie R. Koval.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983
  • Vertical drop test of a transport fuselage section located forward of the wing [microform] / M. Susan Williams and Robert J. Hayduk.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS100711

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