Title

Landing-Gear Vibration

Date

1951

Index Abstract

Coming Soon

Photo Quality

Complete

Report Number

AF TR 6590

Corporate Author

Flight Research Laboratory

Laboratory

Flight Research Laboratory

PB Number

PB116370

Identifier

ADA955967

ADA955967

Access Rights

Notice(s)

Distribution Classification

1

Contract

Laboratory Research - No Contract

DoD Project

None Given

DoD Task

None Given

DTIC Record Exists

Yes

Distribution Change Authority Correspondence

None

Distribution Conflict

No

Index Price

$3.75

Index In

U.S. Government Research Reports, vol. 23, no. 4, p.147, 4/15/1955

Report Availability

Full text available

Extent

78

Date Modified

Scanned by request 5/30/2008 submitted by Cessna (Aerospace Industry - Domestic)

Abstract

The self-excited vibration of a landing gear is generated in an interplay of effects present in the tire, the landing gear proper, and in the entire airfram itself. The analysis of these simultaneous actions is given a simple form; the manner in which energy enters the system, and the necessary structural modifications to control ahimmy are explained.

Date Issued

1951-10

Provenance

AFRL/VACA

Type

report

Subject

Landing Gear

Vibration

Aerodynamic Forces

Airframes

Format

1 online resource

Creator

Moreland, William J.