The Investigation of Take-off and Landing Characteristics of Jet Shortened Take-off and Landing Aircraft (STOL) (K Voprosu Issledovaniya Vzletno-Posadochnykh Kharakteristik Reaktivnykh Samoletov Ukorochennogo Vzleta i Posadki (SUVP)),

Abstract

The negative effect of secondary forces induced by the jet flow of the engine because of its ejection properties is not taken into account during the examination of aerodynamic and take-off and landing characteristics of jet STOL and VTOL aircraft (vertical take-off and landing aircraft). It can be so significant for certain STOL configurations (Figure 1) that aircraft equipped with a BLC system (boundary layer control) could be more preferable.

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Document Details

Document Type
Technical Report
Publication Date
Jul 25, 1977
Accession Number
ADA044292

Entities

People

  • V. I. Surus

Organizations

  • Office of Naval Intelligence

Tags

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Boundaries
  • Boundary Layer
  • Boundary Layer Control
  • Coefficients
  • Control Systems
  • Engines
  • Flow
  • Jet Aircraft
  • Jet Flow
  • Layers
  • Short Takeoff Aircraft
  • Sustainer Engines
  • Vertical Takeoff Aircraft

Readers

  • Aerospace Engineering
  • Fluid Mechanics and Fluid Dynamics.
  • Information Retrieval