PulseExploreJournal ClubDebatesTrendingResearchersJournals
Instagram
HomeExploreJournal ClubTrending
Synapse
⌘+K
Synapse
April 3, 2026Russian Aeronautics0 citations

Study of the Propulsion Airfoil within the Lifting Fuselage as the Angle of Attack and Intake Airflow Vary

View Full Paper
PBP. V. BulatBaltic State Technical University VoenmehIVI. A. VolobuevBaltic State Technical University Voenmeh

Key Points

  • The research aims to explore the performance limits of a propulsive airfoil under different attack angles and airflow conditions.
  • Analyzed airfoil performance at various angles of attack
  • Examined different intake air volume scenarios
  • Measured changes in lifting force and thrust generation
  • Demonstrated a significant increase in lifting force with varying angles of attack
  • Identified limits on maintaining thrust with constant airflow
  • Revealed critical airflow points influencing airfoil performance

Abstract

This study investigates the performance of a propulsive airfoil, designed to generate thrust, while extracting air at the upper critical point. The analysis covers a range of attack angles, with both constant and varying intake air volumes. The aim of the study was to determine the limits of the effect of the significant increase in the lifting force and the ability to maintain that effect with a constant intake airflow rate.

Ask AI
Helpful
Bookmark
Share
View Full Paper

Cite This Study

Bulat et al. (2025) studied this question.

synapsesocial.com/papers/69cf5de95a333a821460bfe4https://doi.org/10.3103/s1068799825040051
Ask AI
Helpful
Bookmark
Share
View Full Paper