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141
Section data for thin, highly cambered airfoils in incompressible flow /
by Milgram, Jerome H.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1971

Government Document Book
142
Effects of winglets on a first-generation jet transport wing : VII, sideslip effects on winglet loads and selected wing loads at subsonic speeds for a full-span model /
by Meyer, Robert R.
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986

Government Document Book
143
Calculative techniques for transonic flows about certain classes of wing-body combinations /
by Stahara, Stephen S.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book
144
Transonic Navier-Stokes wing solutions using a zonal approach.
by Chaderjian, Neal M.
Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [For sale by the National Technical Information Service], 1986

Government Document Book
145
NACA0012 benchmark model using experimental flutter results with unsteady pressure distributions /
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1992

Government Document Book
146
Boundary-layer measurements on a transonic low-aspect ratio wing /
by Keener, Earl R.
Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [For sale by the National Technical Information Service], 1986

Government Document Book
147
Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /
by Naeseth, Roger L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1970

Government Document Book
148
Analytical heat transfer investigation of insulated liquid methane wing tanks for supersonic cruise aircraft /
by Pleban, Eugene J.
Washington : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Va.], 1970

Government Document Book
149
The aerodynamic design of the oblique flying wing supersonic transport /
by Van der Velden, Alexander J. M.
Palo Alto, Calif. : Moffett Field, Calif. : Stanford University ; National Aeronautics and Space Administration, Ames Research Center, 1990

Government Document Book
150
A Fundamental approach to the sticking of insect residues to aircraft wings /
Hampton, Va. : The Center, 1984

Government Document Book
151
Leading edge vortex dynamics on a pitching delta wing : a thesis /
by LeMay, Scott P.
[Notre Dame, Ind.] : Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, 1988

Government Document Book
152
High angle-of-attack aerodynamic characteristics of crescent and elliptic wings /
by Van Dam, C. P. (Cornelis P.), 1954-
Davis, CA : University of California, Dept. of Mechanical Engineering, Division of Aeronautical Science and Engineering, 1989

Government Document Book
153
Computation technique for compressible vortex flows using the integral equation solution : final report /
by Kandil, Osama A.
Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, College of Engineering, Old Dominion University, 1988

Government Document Book
154
Development of stitched/RTM primary structures for transport aircraft /
by Hawley, Arthur V.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1993

Government Document Book
155
Initial piloted simulation study of geared flap control for tilt-wing V/STOL aircraft /
by Guerrero, Lourdes M.
Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [For sale by the National Technical Information Service], 1991

Government Document Book
156
Detailed analysis and test correlation of a stiffened composite wing panel /
by Davis, D. Dale
Hampton, Va. : [St. Louis, Mo.] : National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, Aviation R & T Activity, 1991

Government Document Book
157
Factors affecting the sticking of insects on modified aircraft wings : semi-annual report, June 15, 1986 to December 30, 1986 /
Blacksburg, Va. : [Washington, D.C.] : [Springfield, Va.] : Virginia Polytechnic Institute and State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1987

Government Document Book
158
Evaluation of cloud detection instruments and performance of laminar-flow leading-edge test articles during NASA leading-edge flight-test program /
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [National Technical Information Service, distributor], 1989

Government Document Book
159
Stability and control characteristics of a large-scale deflected slipsteam STOL model with a wing of 5.7 aspect ratio /
by Page, V. Robert
Washington, D.C. : National Aeronautics and Space Administration, 1971

Government Document Book
160
Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /
by Mack, Robert J.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1988

Government Document Book
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