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1
A survey of computational aerodynamics in the United States /
by Gessow, Alfred
Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration , Scientific and Technical Information Office ; For sale by the National Technical Information Service], 1977

Government Document Book
2
Analysis of stability contributions of high dihedral V-trails /
by Freeman, Carl E., Yeager, William T.
[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
3
A study of panel loads and centers of pressure of three different cruciform aft-tail control surfaces of a wingless missile from March 1.60 to 3.70 /
by Lamb, Milton
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980

Government Document Book
4
Exploratory studies of the cruise performance of upper surface blown configurations : summary report /
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980

Government Document Book
5
Aerodynamic properties of a flat plate with cavity for optical-propagation studies /
by Buell, Donald A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1979

Government Document Book
6
Static aerodynamic characeristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63 /
by Freeman, Delma C., Fournier, Roger H.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Information Service, 1977

Government Document Book
7
An analysis of the gust-inducesd overspeed trends of helicopter rotors /
by Jenkins, Julian L., Yeager, William T.
[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
8
Development and validation of a combined rotor-fuselage induced flow-field computational method /
by Freeman, Carl E.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980

Government Document Book
9
Mean velocity, turbulence intensity, and scale in a subsonic turbulence jet impinging normal to a large flat plate /
by Boldman, Donald R.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977

Government Document Book
10
A FORTRAN program for calculating three-dimensional, inviscid, rotational flows with shock waves in axial compressor blade rows : user's manual /
by Thompkins, William T.
Washington, D.C. : [Springfield, Va.] : National Aeronautical and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1982

Government Document Book
11
Helicopter blade dynamic loads measured during performance testing of two scaled rotors /
by Berry, John D.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987

Government Document Book
12
Wind-tunnel tests of wide-chord teetering rotors with and without outboard flapping hinges /
by Weller, William H., Lee, Bill L.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977

Government Document Book
13
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
14
An experimental investigation of two large annular diffusers with swirling and distorted inflow /
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1980

Government Document Book
15
Analytical study of a free-wing/free-trimmer concept /
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
The incorporation of plotting capability into the "unified subsonic supersonic aerodynamic analysis program", version B /
by Winter, Octavio A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by National Technical Information Service], 1980

Government Document Book
17
Supersonic aerodynamic characteristics of a Sparrow III type missile model with wing controls and comparison with existing tail-control results /
by Monta, William 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
18
A three dimensional vortex wake model for missiles at high angles of attack /
by Sheffield, J. Steven
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980

Government Document Book
19
Calculation of two-dimensional inlet flow fields in a supersonic free stream : program documentation and test cases /
by Biringen, Sedat
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980

Government Document Book
20
Effects of primary rotor parameters on flapping dynamics /
by Chen, Robert T. N.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980

Government Document Book
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