Reducing Propulsion Airframe Aeroacoustic Interactions With Uniquely Tailored Chevrons: 2. Installed Nozzles

doi 10.2514/6.2006-2434
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

Unstructured CFD and Noise Prediction Methods for Propulsion Airframe Aeroacoustics

2006English

A Three-Dimensional Vortex Particle-Panel Method for Modeling Propulsion-Airframe Interaction

2010English

Uniquely Clean 2×2 Invertible Integral Matrices

Studia Universitatis Babes-Bolyai Mathematica
Mathematics
2017English

Initial Flight Operations of the Miniature Propulsion System Installed on Small Space Probe: PROCYON

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
2016English

Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point

2016English

Reducing Warfarin Medication Interactions

Archives of Internal Medicine
2006English

Culturally Tailored Intervention for Rural African Americans With Type 2 Diabetes

Diabetes Educator
Health ProfessionsDiabetesMetabolismEndocrinology
2008English

Reducing the H0 and Σ8 Tensions With Dark Matter-Neutrino Interactions

Physical Review D
AstronomyPhysics
2018English

Aeroacoustic Measurement With Combined Proper Orthogonal Decomposition Analysis

TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
2013English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy