Research Catalog

Title

Improving CPA-TSD steady pressure solutions through airfoil slope modification [microform] / Kent F. Mitterer ... [et al.].

Publication

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]

Details

Additional Authors

• Mitterer, Kent F.
• Langley Research Center.

Description

1 v.

Series Statement

NASA technical memorandum ; 110214

Alternative Title

Improving CPA TSD steady pressure solutions through airfoil slope modification

Subject

• Computer aided design
• Computerized simulation
• Airfoil profiles
• Aeroelasticity
• Leading edges

Note

• Distributed to depository libraries in microfiche.
• Shipping list no.: 97-0681-M.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.15:110214

OCLC

marcive37496170

Title

Improving CPA-TSD steady pressure solutions through airfoil slope modification [microform] / Kent F. Mitterer ... [et al.].

Imprint

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]

Series

NASA technical memorandum ; 110214

Reproduction

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

Added Author

Mitterer, Kent F.

Langley Research Center.

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:110214

Research Call Number

READEX Microfiche NAS 1.15:110214