Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("CHARGE AERODYNAMIQUE")

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 28

  • Page / 2
Export

Selection :

  • and

UNSTEADY AERODYNAMIC MODELING FOR ARBITRARY MOTIONS.EDWARDS JW.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 4; PP. 593-595; BIBL. 6 REF.Article

RECENT DEVELOPMENTS IN PREDICTING UNSTEADY AIRLOADS CAUSED BY CONTROL SURFACE MOTIONS.ROWE WS; SEBASTIAN JD; REDMAN MC et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 12; PP. 955-961; BIBL. 9 REF.Article

AERODYNAMIC LOADING ON HIGH-SPEED GROUND VEHICLES = CHARGES AERODYNAMIQUES SUR DES VEHICULES TERRESTRES A HAUTE VITESSECRIMI P; JOHNSON RA.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 317-318; BIBL. 6 REF.Serial Issue

WIND TUNNEL TEST TECHNIQUES FOR THE MEASUREMENT OF UNSTEADY AIRLOADS ON OSCILLATING LIFTING SYSTEMS AND FULL SPAN MODELS.FORSCHING H.1975; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 51; PP. 1-51; ABS. ALLEM.; BIBL. 1 P.Serial Issue

DOUBLET LATTICE METHOD-SCHEMES FOR CPU TIME REDUCTIONSIMHA PRASAD DS; HOLLA VS.1980; COMPUTER METHODS APPL. MECH. ENGNG; NLD; DA. 1980; VOL. 23; NO 1; PP. 59-65; BIBL. 4 REF.Article

A SENSITIVE ROLLING MOMENT BALANCE FOR USE IN SUPERSONIC BLOWDOWN TUNNELSSUNDARA MURTHY H.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 9; PP. 799-800; BIBL. 3 REF.Article

LOAD DISTRIBUTIONS ON SLENDER DELTA WINGS HAVING VORTEX FLOW.KUHLMAN J.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 699-702; BIBL. 8 REF.Article

PREDICTION OF AERODYNAMIC LOADING. FLUID DYNAMICS PANEL SYMPOSIUM. PAPERS AND DISCUSSIONS; AMES, MOFFETT FIELD, CALIF.; 1976.1977; A.G.A.R.D. CONF. PROC.; FR.; DA. 1977; NO 204; PP. (328P.); BIBL. DISSEM.Conference Paper

STRUCTURAL TESTS OF AERODYNAMIC SURFACES: A SYSTEM APPROACH TO ANALYSIS AND DESIGN.GOLDENBERG K.1976; J. TESTG. EVAL.; U.S.A.; DA. 1976; VOL. 4; NO 6; PP. 418-424; BIBL. 7 REF.Article

ANALYSIS OF VALIDATION TEST OF THE LANGLEY PILOT TRANSONIC CRYOGENIC TUNNEL.RAY EJ; KILGORE RA; ADCOCK JB et al.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 6; PP. 539-544; BIBL. 4 REF.Article

AGARD TWO-DIMENSIONAL AEROELASTIC CONFIGURATIONSBLAND SR.1979; ; FRA; DA. 1979; AGARD-AR 156; IV-10 P.: ILL.; 30 CM; BIBL. 10 REF.; ISBN 92-835-1333-9Report

MECANIQUE DES GRILLES D'AUBES PLANES.COMOLET R.1974; ELECTR. FR., BULL. DIRECT. ET. RECH., A; FR.; DA. 1974; NO 2; PP. 1-104; ABS. ANGL.; BIBL. 1 P. 1/2Article

FLOW AROUND FIXED CIRCULAR CYLINDERS: FLUCTUATING LOADSFARELL C.1981; PROC. AM. SOC. CIV. ENG., J. ENG. MECH. DIV.; ISSN 0044-7951; USA; DA. 1981; VOL. 107; NO 3; PP. 565-588; BIBL. 67 REF.Article

UNSTEADY AIRLOADS IN SUPERCRITICAL TRANSONIC FLOWSWILLIAMS MH.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 2; PP. 135-140; BIBL. 10 REF.Article

VORTEX-INDUCED ASYMMETRIC LOADS IN Z-D AND 3-D FLOWSERICSSON LE; REDING JP.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 45 P.; BIBL. 136 REF.Conference Paper

QUELQUES PROBLEMES AERODYNAMIQUES DES VOITURES PARTICULIERESMARYNIAK J.1975; ARCH. BUDOWY MASZ.; POLSKA; DA. 1975; VOL. 22; NO 3; PP. 271-288; ABS. RUSSE ANGL.; BIBL. 10REF.Article

BENDING-TORSIONAL FLUTTER OF A CANTILEVERED WING CONTAINING A TIP MASS AND SUBJECTED TO A TRANSVERSE FOLLOWER FORCE.FELDT WT; HERRMANN G.1974; J. FLANKLIN INST.; U.S.A.; DA. 1974; VOL. 297; NO 6; PP. 467-478; BIBL. 14 REF.Article

CALCULATION OF UNSTEADY SUBSONIC FLOW ABOUT HARMONICALLY OSCILLATING WING/BODY CONFIGURATIONS.ROOS R; BENNEKERS B; ZWAAN RJ et al.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 5; PP. 447-454; BIBL. 13 REF.Article

THE ESTIMATION OF EXTREME WINDSMAYNE JR.1979; J. INDUSTR. AERODYN.; NLD; DA. 1979; VOL. 5; NO 1-2; PP. 109-137; BIBL. 18 REF.Article

AEROELASTICITY OF ROTARY WING AIRCRAFT = AEROELASTICITE D'AVIONS A VOILURE TOURNANTEDAT R.1973; AGARD-LS-63; FR.; DA. 1973; PP. 4.1-4.33; BIBL. 1 P.; (HELICOPTER AERODYN. DYN.; BRUSSELS; 1973)Conference Proceedings

TRANSONIC SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON AN OSCILLATING AIRFOILDAVIS SS; MALCOLM GN.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 11; PP. 1306-1312; BIBL. 27 REF.Article

COMPUTER OPTIMIZATION OF HYDRAULIC SYSTEM PRESSURE FOR DEVELOPMENT AND QUALIFICATION TESTING.GOLDENBERG K; COLLINS DG.1974; J. TESTG EVAL.; U.S.A.; DA. 1974; VOL. 2; NO 4; PP. 229-234; BIBL. 6 REF.Article

ROTOR UNSTEADY AIRLOADS1973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 111; PP. (46 P.); ABS. ANGL.; BIBL. DISSEM.; (AERODYN. ROTARY WINGS. FLUID DYN. PANEL SPEC. MEET. PAP.; MARSEILLE; 1972)Conference Paper

EEC-SPONSORED THEORETICAL STUDIES OF GAS CLOUD EXPLOSION PRESSURE LOADINGS: FINAL REPORTBRISCOE F; GURTRESS N; FARMER CL et al.1979; ; LUX; LUXEMBOURG: CCE; DA. 1979; EUR 6119; 120 P.; 30 CM; ISBN 92-825-0805-6; NUCLEAR SCIENCE AND TECHNOLOGYReport

Sensitivity analysis of unsteady aerodynamic loads in cascadesLORENCE, C. B; HALL, K. C.AIAA journal. 1995, Vol 33, Num 9, pp 1604-1610, issn 0001-1452Conference Paper

  • Page / 2