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Inlets for Supersonic Missiles

Inlets for Supersonic Missiles PDF Author: John J. Mahoney
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 264

Book Description
This book describes the design, operation, performance, and selection of the inlets (also known as intakes and air-induction systems) indispensable to proper functioning of an airbreathing engine. Topics include functions and fundamentals, supersonic diffusers, subsonic diffusers, viscous effects, operational characteristics, performance estimation, installation factors, variable geometry, and proof of capability.

Inlets for Supersonic Missiles

Inlets for Supersonic Missiles PDF Author: John J. Mahoney
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 264

Book Description
This book describes the design, operation, performance, and selection of the inlets (also known as intakes and air-induction systems) indispensable to proper functioning of an airbreathing engine. Topics include functions and fundamentals, supersonic diffusers, subsonic diffusers, viscous effects, operational characteristics, performance estimation, installation factors, variable geometry, and proof of capability.

Shoreline Erosion and Storm Damages at Lake Worth Inlet, Palm Beach Harbor, Florida

Shoreline Erosion and Storm Damages at Lake Worth Inlet, Palm Beach Harbor, Florida PDF Author: United States. Office of the Assistant Secretary of the Army (Civil Works)
Publisher:
ISBN:
Category : Beach erosion
Languages : en
Pages : 612

Book Description


Hydraulics of Closed Conduit Spillways; Part XII: The Two-way Drop Inlet with a Flat Bottom

Hydraulics of Closed Conduit Spillways; Part XII: The Two-way Drop Inlet with a Flat Bottom PDF Author: Charles A. Donnelly
Publisher:
ISBN:
Category : Aqueducts
Languages : en
Pages : 80

Book Description


Brigantine Inlet to Great Egg Harbor Inlet

Brigantine Inlet to Great Egg Harbor Inlet PDF Author: United States. Army. Corps of Engineers. Philadelphia District
Publisher:
ISBN:
Category : Absecon Island (N.J.)
Languages : en
Pages : 1130

Book Description


Brigantine Inlet to Great Egg Harbor Inlet Feasibility Study

Brigantine Inlet to Great Egg Harbor Inlet Feasibility Study PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 250

Book Description


Moriches Inlet Navigation Improvements

Moriches Inlet Navigation Improvements PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 346

Book Description


A Comparison of the Performance of Four Side-mounted Inlets Over a Mach Number Range of 0.88 to 2.2 and Angles of Attack to 14°

A Comparison of the Performance of Four Side-mounted Inlets Over a Mach Number Range of 0.88 to 2.2 and Angles of Attack to 14° PDF Author: Leroy L. Presley
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 58

Book Description


Fire Island Inlet to Montauk Point, Long Island, Reach 1, New York, Fire Island Inlet to Moriches Inlet, Evaluation of an Interim Plan for Storm Damage Reduction

Fire Island Inlet to Montauk Point, Long Island, Reach 1, New York, Fire Island Inlet to Moriches Inlet, Evaluation of an Interim Plan for Storm Damage Reduction PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 1070

Book Description


Investigation at Supersonic and Subsonic Mach Numbers of Auxiliary Inlets Supplying Secondary Air Flow to Ejector Exhaust Nozzles

Investigation at Supersonic and Subsonic Mach Numbers of Auxiliary Inlets Supplying Secondary Air Flow to Ejector Exhaust Nozzles PDF Author: Donald P. Hearth
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52

Book Description
The results indicated increases in auxiliary-inlet pressure recovery with increases in scoop height relative to the boundary-layer thickness. The pressure recovery increased at about the same rate as theoretically predicted for an inlet in a boundary layer having a one-seventh power profile, but was only about 0.68 to 0.75 of the theoretically obtainable values. Under some operating conditions, flow from the primary jet was exhausted through the auxiliary inlet. This phenomenon could be predicted from the ejector pumping characteristics.

Characteristic Design Study of Mixed-compression Two-dimensional Inlets with Low-angle Cowls for the Mach Number Range 2.70 to 1.80

Characteristic Design Study of Mixed-compression Two-dimensional Inlets with Low-angle Cowls for the Mach Number Range 2.70 to 1.80 PDF Author: Bernhard H. Anderson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42

Book Description