LOADS EXPERIENCED IN FLIGHTS OF TWO SWEPT-WING RESEARCH AIRPLANES IN THE ANGLE-OF-ATTACK RANGE OF REDUCED STABILITY

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Document Details

Document Type
Technical Report
Publication Date
Jun 05, 1953
Accession Number
AD0011100

Entities

People

  • Albert E. Kuhl
  • Glenn H. Robinson
  • Hubert M. Drake

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Airframes
  • Airplanes
  • Altitude
  • Angular Acceleration
  • Bending Moments
  • Boundaries
  • High Altitude
  • High Angles
  • High Lift
  • Horizontal Stabilizers
  • Mach Number
  • Measurement
  • Research Aircraft
  • Structural Loads
  • Swept Wings