Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters
By: Cynthia A. Crowell and Henry L. Kelley.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 4248.; AVSCOM technical report -- 90-B-010.; AVSCOM technical report -- 90-B-10.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; National Technical Information Service, distributor
Published: 1990
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Cross flow.; helicopter control.; Helicopter performance.; Strakes.; Tail assemblies.; Wind direction.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.