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Optimal pitch thrust-vector angle and benefits for all flight regimes [microform] / Glenn B. Gilyard, Alexander Bolonkin.
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 2000]
2000
0 resources
Development of a mulicomponent force and moment balance for water tunnel applications [microform] / Carlos J. Suárez ... [et al.].
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
1994
0 resources
Development of an advanced pitch active control system for a wide body jet aircraft [microform] / Wiley A. Guinn, Jerry J. Rising, and Walt J. Davis.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1984]
1984
0 resources
Development of an advanced pitch active control system and a reduced area horizontal tail for a wide body jet aircraft [microform] : executive summary / Wiley A. Guinn.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1984]
1984
0 resources
An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities [microform] / C.L. Blanken, H.-J. Pausder and C.J. Ockier.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Design and dynamic simulation of a fixed pitch 56 kW wind turbine drive train with a continuously variable transmission [microform] / C. Gallo ... [et al.].
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Effects of optical pitch on oculomotor control and the perception of target elevation [microform] / Malcolm M. Cohen, Sheldon M. Ebenholtz, and Barry J. Linder.
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance [microform] / John S. Orme, Ross Hathaway, Michael D. Ferguson.
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations [microform] / Robert M. Bennett and Charlotte E. Walker.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
Swashplate control system [microform].
[Moffett Field, Calif. : NASA Ames Research Center, 1986]
1986
0 resources
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