NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Inlet Performance Characteristics from Wind-Tunnel Tests of a 0.10-Scale Air-Induction System Model of the YF-108A Airplane at Mach Numbers of 2.50, 2.76, and 3.00Inlet-performance and external-drag-coefficient characteristics are presented without analysis. Effects are shown of variations of fuselage boundary-layer diverter profile, bleed-surface porosity, bleed-exit area, and inlet ramp, and lip angle.
Document ID
19980228132
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Blackaby, James R. (NASA Ames Research Center Moffett Field, CA United States)
Lyman, E. Gene (NASA Ames Research Center Moffett Field, CA United States)
Altermann, John A., III (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-MEMO-7-18-59A
AF-AM-157
Report Number: NASA-MEMO-7-18-59A
Report Number: AF-AM-157
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available