Improving CPA-TSD steady pressure solutions through airfoil slope modification
By: Kent F. Mitterer ... [et al.].
Contributors: Mitterer, Kent F.; Langley Research Center.
Series: NASA technical memorandum -- 110214.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Computer aided design; Computerized simulation; Airfoil profiles; Aeroelasticity; Leading edges
Other titles: Improving CPA TSD steady pressure solutions through airfoil slope modification.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 97-0681-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.