Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2
By: D. R. Boldman ... [et al.].
Contributors: Boldman, Donald R.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 104428.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1991
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Ducts.; Engine inlets.; Low speed wind tunnels.; Panel method (Fluid dynamics).; Shrouded propellers.; Simulators.; Subsonic speed.
Notes: Distributed to depository libraries in microfiche.

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