THE EFFECTS OF STRAIN AND TEMPERATURE ON THE DYNAMIC PROPERTIES OF ELASTOMERSDARLOW MS; SMALLEY AJ.1980; J. MECH. DESIGN; USA; DA. 1980; VOL. 102; NO 1; PP. 45-53; BIBL. 8 REF.Article

TORSIONAL STABILITY ANALYSIS OF A GAS-TURBINE POWERED HELICOPTER DRIVE SYSTEMDARLOW MS; VANCE JM.1974; J. ENGNG POWER; U.S.A.; DA. 1974; VOL. 96; NO 4; PP. 335-341; BIBL. 9 REF.Article

APPLICATION OF THE PRINCIPLE OF RECIPROCITY TO FLEXIBLE ROTOR BALANCINGDARLOW MS; SMALLEY AJ.1982; J. MECH. DES.; ISSN 0161-8458; USA; DA. 1982; VOL. 104; NO 2; PP. 329-333; BIBL. 7 REF.Article

A UNIFIED APPROACH TO FLEXIBLE ROTOR BALANCING: OUTLINE AND EXPERIMENTAL VERIFICATIONDARLOW MS; SMALLEY AJ; PARKINSON AG et al.1980; VIBRATIONS IN ROTATING MACHINERY. INTERNATIONAL CONFERENCE. 2/1980/CAMBRIDGE; GBR; LONDON: MECHANICAL ENGINEERING PUBLICATIONS; DA. 1980; PP. 437-444; BIBL. 13 REF.Conference Paper

THE DYNAMIC CHARACTERISTICS OF O-RINGS.SMALLEY AJ; DARLOW MS; MEHTA RK et al.1978; J. MECH. DESIGN; USA; DA. 1978; VOL. 100; NO 1; PP. 132-138; BIBL. 6 REF.Article

ACOUSTIC EMISSION DETECTION OF FATIGUE CRACK INITIATION AND PROPAGATION IN NOTCHED AND UNNOTCHED TITANIUM SPECIMENS.SHINAISHIN OA; DARLOW MS; ACQUAVIVA SJ et al.1976; MATER. EVALUAT.; U.S.A.; DA. 1976; VOL. 34; NO 6; PP. 137-143; BIBL. 6 REF.Article

DEMONSTRATION OF A UNIFIED APPROACH TO THE BALANCING OF FLEXIBLE ROTORSDARLOW MS; SMALLEY AJ; PARKINSON AG et al.1981; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1981; VOL. 103; NO 1; PP. 101-107; BIBL. 12 REF.Article

EXTENSION OF THE TRANSFER MATRIX METHOD FOR ROTORDYNAMIC ANALYSIS TO INCLUDE A DIRECT REPRESENTATION OF CONICAL SECTIONS AND TRUNNIONSDARLOW MS; MURPHY BT; ELDER JA et al.1980; J. MECH. DESIGN; USA; DA. 1980; VOL. 102; NO 1; PP. 122-129; BIBL. 6 REF.Article