Evaluation by step response tests of prototype relief valves designed for YF-12 inlet stability bleed system /
Miles O. Dustin and George H. Neiner.

Description

Main Author: Dustin, Miles O.
Related Names: Neiner, George H.
Lewis Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1975.
Subjects: SR-71 Blackbird (Jet reconnaissance plane)
Aerodynamics, Supersonic.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Air intakes > Airplanes / Turbojet engines / Air intakes / Automatic control.
Airplanes > Airplanes / Air ducts > Airplanes / Air ducts / Automatic control.
Note: Prepared at Lewis Research Center.
Cover title.
Physical Description: 44 p. : ill. ; 27 cm.
Locate a Print Version: Find in a library

Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign