Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane /

Bibliographic Details
Main Authors:	Hughes, Donald L. (Donald Lee), 1926- (Author), Myers, Lawrence P. (Author), Mackall, Karen G. (Author)
Corporate Authors:	Ames Research Center, Hugh L. Dryden Flight Research Center
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Series:	NASA technical paper ; 2411.
Subjects:	Static pressure. Aircraft engines. Inlet flow. Flight tests. Pressure measurement. Static pressure probes > Testing. Airplanes > Turbojet engines > Air intakes. Eagle (Jet fighter plane)
Online Access:	https://purl.fdlp.gov/GPO/gpo93432

Description
Item Description:	"April 1985." Prepared at the Dryden Flight Research Facility.
Physical Description:	1 online resource (20 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 6).