A successful step toward an advanced supersonic transport engine - Acoustic and emission results from the Pratt and Whitney Aircraft Variable Cycle Engine Program-Reference-Cited by-同舟云学术

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A successful step toward an advanced supersonic transport engine - Acoustic and emission results from the Pratt and Whitney Aircraft Variable Cycle Engine Program

Published:1981-07-27 Issue: Volume: Page:
ISSN:
Container-title:17th Joint Propulsion Conference
language:
Short-container-title:

Author:

WESTMORELAND J.¹,PACKMAN A.¹

Affiliation:

1. United Technologies Corp., Pratt and Whitney Aircraft Group, East Hartford, CT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1593

Reference13 articles.

1. Sabatella, J.A. "Advanced Supersonic Propulsion Study - Phase I,"Final Report NASA CR-134633, January 1974.

2. Howlett R.A., J.A. Sabatella, J. Johnson, and 1. Sewall, "Advanced , Supersonic Propulsion Study - Phase 111, Final Report NASA CR-135148. December 1976.

3. Howlett, R.A., and F.D. Streicher, "l\$vanced Supersonic Propulsion Study - Phase IV, Final Report NASA CR-I 35273. December 1976.

4. Larson, R.S., D.P. Nelson, and B.S. Stevens, "Aerodynamic and Acoustic Investigation of Inverted Velocity Profile Coannular Exhaust Nozzle Models and Development of Aerodynamic and Acoustic Prediction Procedures." NASA CR-3168.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design method of optimal control schedule for the adaptive cycle engine steady-state performance;Chinese Journal of Aeronautics;2022-04

2. The challenge of reducing supersonic civil transport propulsion noise;25th Joint Propulsion Conference;1989-07-12

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