Cover Image

Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration /

Bibliographic Details
Main Author: Kemmerly, Guy T.
Corporate Authors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, Langley Research Center
Format: Government Document Microform Book
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1990.
Series:NASA technical paper ; 3000.
Subjects:
Aerodynamic characteristics.
Aircraft configurations.
Aircraft landing.
F-15 aircraft.
Ground effect (Aerodynamics)
Ground tests.
Short takeoff aircraft.
Online Access:https://purl.fdlp.gov/GPO/LPS68080
Description
Item Description:"June 1990."
Prepared at Langley Research Center.
Shipping list number: 1991-0132-M.
Distributed to depository libraries in microfiche.
Microform.
Physical Description:28 pages : illustrations ; 28 cm.
Also available via Internet from the NTRS web site. Address as of 3/23/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900013215%5F1990013215.pdf; current access is available via PURL.
Bibliography:Bibliography: page 12.