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1
Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization
by Carlson, Harry W.
[Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1990

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Government Document Book
2
Calculations, and comparison with an ideal minimum, of trimmed drag for conventional and canard configurations having various levels of static stability /
by McLaughlin, Milton D.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book
3
Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /
by Mason, Mary L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book
4
A look at handling qualities of canard configurations /
by Anderson, Seth B.
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
5
Effect of canard vertical location, size, and deflection on canard-wing interference at subsonic speeds /
by Gloss, Blair B., Ray, Edward J., Washburn, Karen E.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book
6
Approximate neutral point of a subsonic canard aircraft /
by Phillips, James D.
Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [For sale by the National Technical Information Service], 1985

Government Document Book
7
Wind-tunnel investigation of a full-scale canard-configured general aviation airplane /
by Yip, Long P.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1985

Government Document Book
8
Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /
by Covell, Peter F.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1985

Government Document Book
9
Effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration /
by Gloss, Blair B.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
10
An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90 /
by Re, Richard J., Capone, Francis J.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book
11
Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization /
by Carlson, Harry W.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990

Government Document Book
12
The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 s̊weptback wing at a Mach number of 0.30 /
by Henderson, William P.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
13
X-29A aircraft structural loads flight testing /
Edwards, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [For sale by the National Technical Information Service], 1989

Government Document Book
14
Investigation of the divergence characteristics of delta-planform canard controls /
by Rainey, A. Gerald
Washington, D.C. : National Aeronautics and Space Administration, 1966

Government Document Book
15
Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration /
by Gloss, Blair B.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration : Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book
16
High-angle-of-attack stability characteristics of a three-surface fighter configuration /
by Grafton, Sue B.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book
17
High angle canard missile test in the Ames 11-foot transonic wind tunnel /
by Schwind, Richard G.
Washington : Springfield, Va. : National Aeronautics and Space Adiministration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book
18
Low-speed investigation of effects of wing leading- and trailing-edge flap deflections and canard incidence on a fighter configuration equipped with a forward-swept wing /
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984

Government Document Book
19
Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20 /
by Re, Richard J., Capone, Francis J.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book
20
A study of canard-wing interference using experimental pressure data at transonic speeds /
by Gloss, Blair B., Washburn, Karen E.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1979

Government Document Book
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