Optimal pitch thrust-vector angle and benefits for all flight regimes
By: Glenn B. Gilyard, Alexander Bolonkin.
Contributors: Hugh L. Dryden Flight Research Center.
Series: NASA/TM -- 2000-209021; NASA technical memorandum -- 2000-209021.
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; National Technical Information Service, distributor
Published: 2000
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Number of pages: 22
Subjects: Airplanes -- Control surfaces.; Airplanes -- Flight testing.; Airplanes -- Handling characteristics.; Airplanes -- Motors -- Thrust.; Drag (Aerodynamics); Lift (Aerodynamics)
Notes: "March 2000."

"Performing organization report number H-2402"--Report documentation page.

Includes bibliographical references.

Performed by NASA Dryden Flight Research Center for National Aeronautics and Space Administration WU 522-16-14-00-39-00-LIO