Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3 /
Allen B. Henning.

Description

Main Author

Henning, Allen B.

Related Names

United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, [1957]

Subjects

Charts, diagrams, etc.
Mach number.
Stability.
Drag (Aerodynamics)
Lift (Aerodynamics)
Aerofoils > Aerofoils / Testing.

Summary

An investigation was made to determine the effects of wing inboard plan-form modifications on the lift, drag, and longitudinal characteristics of a rocket-propelled free-flight model. The model had a body of fineness ration 17.4, a modified wing with a basic plan form swept back 52.5 degrees and an aspect ratio of 3, and inline horizontal tail surfaces which were aerodynamically pulsed continuously throughout the flight.

Note

NACA Research Memorandum L57D29.
"June 19, 1957."
Title from cover.

Physical Description

24 p. : ill. ; 27 cm.

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