FLIGHT INVESTIGATION OF THE EFFECT OF A PROPULSIVE JET POSITIONED ACCORDING TO THE TRANSONIC AREA RULE ON THE DRAG COEFFICIENTS OF A SINGLE-ENGINE DELTA-WING CONFIGURATION AT MACH NUMBERS FROM 0.83 TO 1.36

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 13, 1956
Accession Number
AD0093275

Entities

People

  • Joseph H. Judd
  • Ralph A. Falanga

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Base Pressure
  • Center Of Gravity
  • Combustion
  • Combustion Chambers
  • Delta Wings
  • Drag
  • Dynamic Pressure
  • Flight Instruments
  • Flow Fields
  • Mach Number
  • Measurement
  • Simulators
  • Static Pressure
  • Telemetry Equipment
  • Turbojet Engines