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portada Design and Evaluation of a Turbojet Exhaust Simulator, Utilizing a Solid-Propellant Rocket Motor, for Use in Free-Flight Aerodynamic Research Models
Type
Physical Book
Publisher
Language
English
Pages
30
Format
Paperback
Dimensions
24.6x18.9x0.2 cm
Weight
0.07 kg.
ISBN13
9781289264192

Design and Evaluation of a Turbojet Exhaust Simulator, Utilizing a Solid-Propellant Rocket Motor, for Use in Free-Flight Aerodynamic Research Models

Nasa Technical Reports Server (Ntrs) (Author) · Carlos a. Demoraes (Author) · Bibliogov · Paperback

Design and Evaluation of a Turbojet Exhaust Simulator, Utilizing a Solid-Propellant Rocket Motor, for Use in Free-Flight Aerodynamic Research Models - Demoraes, Carlos a. ; Nasa Technical Reports Server (Ntrs) ; Et Al

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Delivery: 19 Oct - 30 Oct Shipping: 16 to 20 business days.
R 394
R 394

Synopsis "Design and Evaluation of a Turbojet Exhaust Simulator, Utilizing a Solid-Propellant Rocket Motor, for Use in Free-Flight Aerodynamic Research Models"

A method has been developed for modifying a rocket motor so that its exhaust characteristics simulate those of a turbojet engine. The analysis necessary to the design is presented along with tests from which the designs are evaluated. Simulation was found to be best if the exhaust characteristics to be duplicated were those of a turbojet engine at high altitudes and with the afterburner operative.

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