A linear control design structure to maintain loop properties during limit operation in a multi-nozzle turbofan engine
By: Duane Mattern and Peter Ouzts.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 105163
Publisher: National Aeronautics and Space Administration
Published: 1991
Place of publication: [Washington, DC]
Language: eng
Format: Microform
Subjects: Linear systems.; Airplanes -- Turbofan engines.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-501-M.

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