Proceedings of the Technical Conference on the Effects of Helicopter Downwash on Free Projectiles, held at Bridgeton, Missouri, on 12-14 August 1975

Abstract

Partial contents: The Perturbed Flow Environment about Helicopters and its Effect on Free Rockets; Some Practical Aspects of Rotor Wake Effects on Rocket Accuracy; AH-1G Helicopter Field Flow Survey; Total QE Component Variation under Hover Downwash Conditions for Long Range Targets (3-6km); The Effects of Rotor-Wake on Rockets; Rotor-Wake Induced Flow along Helicopter Rocket Trajectories; Analysis of Effects of Calculated Downwash Distribution on Flight Performance of the 2.75-inch Rocket; Measurement of Helicopter Air Data Using Surveilling Pitot Static Pressure Probes; Correlation of Actual Induced Flow with Theory for Bell NUH-1M Helicopter Rotor Operating in Level Flight; Review of LORAS Characteristics; General Requirements for Omni Directional Low Range Airspeed System; LORAS Displays; Ultrasonic Wind Vector Sensor; Application of Remote Wind Sensors; Effects of Airflow on Jettison of Multi- Track Launchers from Helicopters; and VA 210-220 Series, Low Speed Indicator, 1 to 150k and Air Speed/Directional Sensor, 2 Axis, VT1003.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1975
Accession Number
ADA058123

Entities

Organizations

  • United States Army Aviation and Missile Command

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computer Programs
  • Fire Control Systems
  • Fixed Wing Aircraft
  • Flight Speeds
  • Fluid Dynamics
  • Measurement
  • Munitions Testing
  • Rotary Wing Aircraft
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fluid Dynamics.