Aeropropulsive Characteristics of Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model PDF Download

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Aeropropulsive Characteristics of Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model

Aeropropulsive Characteristics of Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model PDF Author: Francis J. Capone
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

Book Description


Aeropropulsive Characteristics of Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model

Aeropropulsive Characteristics of Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model PDF Author: Francis J. Capone
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 402

Book Description


Aeropulsive Characteristics at Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model

Aeropulsive Characteristics at Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model PDF Author: Francis J. Capone
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 84

Book Description
An investigation to determine the aeropropulsive characteristics of nonaxisymmetric nozzles on an F-18 jet effects model was conducted in the Langley 16-foot transonic tunnel and the AEDC 16-foot supersonic wind tunnel. The performance of a two dimensional convergent-divergent nozzle, a single expansion ramp nozzle, and a wedge nozzle was compared with that of the baseline axisymmetric nozzle. Test data were obtained at static conditions and at Mach numbers from 0.60 to 2.20 at an angle of attack of 0 deg. Nozzle pressure ratio was varied from jet-off to about 20.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1282

Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Effect of Varying Internal Geometry on the Static Performance of Rectangular Thrust-reverser Ports

Effect of Varying Internal Geometry on the Static Performance of Rectangular Thrust-reverser Ports PDF Author: Richard J. Re
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 108

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 418

Book Description


NASA Scientific and Technical Publications

NASA Scientific and Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 62

Book Description


Static Internal Performance of a Single-engine Onaxisymmetric-nozzle Vaned-thrust-reverser Design with Thrust Modulation Capabilities

Static Internal Performance of a Single-engine Onaxisymmetric-nozzle Vaned-thrust-reverser Design with Thrust Modulation Capabilities PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 116

Book Description


Vectored Propulsion, Supermaneuverability and Robot Aircraft

Vectored Propulsion, Supermaneuverability and Robot Aircraft PDF Author: Benjamin Gal-Or
Publisher: Springer Science & Business Media
ISBN: 1461389615
Category : Technology & Engineering
Languages : en
Pages : 277

Book Description
This book is designed to fill a professional vacuum in the new field of advance, high-angle, vectored stealth aircraft. The subject matter presented in the volume has never before been investigated and presented as a unified field of study because it covers entirely new fields and because specialized fragments of this unified field are scattered throughout literature in specific problems. The book is of interest to aeronautical and mechanical engineers, electrical and control engineers, aerospace industry, USAF, US Navy, NASA, pilots and instructors.

Aeropropulsive Characteristics of Canted Twin Pitch-vectoring Nozzles at Mach 0.20 to 1.20

Aeropropulsive Characteristics of Canted Twin Pitch-vectoring Nozzles at Mach 0.20 to 1.20 PDF Author: Francis J. Capone
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 264

Book Description