Author: Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 702
Book Description
NACA Conference on Aircraft Loads, Structures, and Flutter
Author: NASA Technical Note
Author: Effects on Adjacent Surfaces from the Firing of Rocket Jets
Author: Walter E. BressettePublisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 14
Book Description
This paper is a preliminary and brief account of some research currently being conducted to determine the jet effects on adjacent surfaces from the firing of rocket jets. Measurements of jet-effect pressures on a flat plate as well as shadowgraphs are presented that were obtained when a rocket jet at a Mach number of 3 was exhausted downstream and upstream into free-stream flow at a Mach number of 2 located from 2 to 4.7 rocket-jet-exit diameters from the plate. The jet effects on the flat plate with the rocket jet exhausting downstream are of the same order of magnitude as those previously obtained from sonic exits with a total pressure 10 times lower. A maximum pressure coefficient on the plate of 1.35 was obtained when the rocket jet was exhausted upstream at 2 rocket-jet-exit diameters below the plate, and an integration of the measured jet-effect pressures at this position resulted in a normal force on the plate equal to 2.3 times the thrust output of the rocket jet.
Jet Effects on Cylindrical Afterbodies Housing Sonic and Supersonic Nozzles which Exhaust Against a Supersonic Stream at Angles of Attack from 90 ̊to 180 ̊
Author: Lovick O. HaymanPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 54
Book Description
Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1116
Book Description
Index to NASA Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Loads Induced on a Flat-plate Wing by an Air Jet Exhausting Perpendicularly Through the Wing and Normal to a Free-stream Flow of Mach Number 2.0
Author: Joseph J. JanosPublisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 26
Book Description
Effect of Nose-mounted Control-system Jets in Roll-control Positions on the Aerodynamics of a Space Vehicle
Author: John T. SuttlesPublisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 34
Book Description
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Author: