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Asymptotic modal analysis and statistical energy analysis

Dowell, E. H.
[Washington, DC : National Aeronautics and Space Administration ; Springfieldl, Va. : For sale by the National Technical Information Service, 1990] 1990

Compressive testing of stitched frame and stringer alternate configurations

Leone, Frank A., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2016. 2016-

Damage arresting composites for shaped vehicles phase II final report

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Estimation of dynamic rotor loads for the rotor systems research aircraft methodology development an

Du Val, R. W.
Mountain View, Calif. : Advanced Rotorcraft Technology, Inc. ; Moffett Field, Calif. : National Aeronautics and Space Administration Ames Research Center, [1985] 1985

Experimental measurement of structural power flow on an aircraft fuselage progress report no. 6, Jan

Cuschieri, J. M. (Joseph M.)
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

Fuselage design for a specified Mach-sliced area distribution

Barger, Raymond L.
[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

Fuselage upwash effects on RSRA rotor systems

Cowan, J.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985] 1985

Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell

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

Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at

Bowman, James S. (James Scarboro), 1924-
[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

Numerical study of three-dimensional separation and flow control at a wing-body junction progress re

Lakshmanan, Balakrishnan, 1957-
Norfolk, Va. : Department of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

PRSEUS acoustic panel fabrication

Velicki, Alex, author.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Study for prediction of rotor/wake/fuselage interference

Clark, D. R.
Redmond, WA : Analytical Methods, Inc. ; Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, [1985] 1985

A study of the utilization of advanced composites in fuselage structures of commercial aircraft fina

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

Transport composite fuselage technology impact dynamics and acoustic transmission

Burbank, Calif. : Lockheed-California Co. ; [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986. 1986