B. M. Jaquet

发表

Simulation of gemini-agena docking

D. R. Riley, B. M. Jaquet, 1964 .

Fixed-base Gemini Agena docking simulation

D. R. Riley, B. M. Jaquet, 1963 .

Analytical Investigation of the Reentry Behavior of the ''flying Wind Tunnel'' Test Vehicle, with Some Effects of Threshold and Torque Level of a Roll-rate Control System

H. S. Fletcher, B. M. Jaquet, 1962 .

STATIC LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS AT A MACH NUMBER OF 3.11 OF SQUARE AND CIRCULAR PLAN-FORM REENTRY VEHICLES, WITH SOME EFFECTS OF CONTROLS AND LEADING-EDGE EXTENSIONS

B. M. Jaquet, 1960 .

Simulation of a landing system for an advanced Apollo-type spacecraft using an all-flexible parawing

G. K. Miller, B. M. Jaquet, D. S. Price, 1967 .

Some Langley Research Center plans in the area of visual displays for lunar mission simulation

D. R. Riley, B. M. Jaquet, 1964 .

A study of Gemini-Agena docking using a fixed-base simulator employing a closed-circuit television system

P. L. Deal, D. R. Riley, B. M. Jaquet, 1965 .

Fixed-base visual simulation of pilot controlled descents of an advanced Apollo spacecraft with an all-flexible parawing

G. K. Miller, B. M. Jaquet, D. B. Price, 1969 .

Effect of target angular oscillations on pilot-controlled Gemini-Agena docking

D. R. Riley, B. M. Jaquet, J. B. Cobb, 1966 .

Simulator studies of space and lunar landing techniques

B. M. Jaquet, 1963 .

Calculated effects of geometric dihedral on the low-speed rolling derivatives of swept wings

B. M. Jaquet, M. Queijo, 1948 .

EFFECT OF LINEAR SPANWISE VARIATIONS OF TWIST AND CIRCULAR-ARC CAMBER ON LOW-SPEED STATIC STABILITY, ROLLING, AND YAWING CHARACTERISTICS OF A 45° SWEPTBACK

B. M. Jaquet, Advisory Committee, 2022 .

Effects of chord discontinuities and chordwise fences on low-speed static longitudinal stability of an airplane model having a 35 degree sweptback wing

Byron M Jaquet, B. M. Jaquet, 1952 .

EFFECTS OF HORIZONTAL-TAIL POSITION AND ASPECT RATIO ON LOW-SPEED STATIC LONGTTUDIMAL STABILITY AND CONTROL CHARACTERBTICS OF A 60° TRIANGULAR-WING MODEL HAVING TWIN TRIANGUUXR.ALL-MOVABLE TAILS

B. M. Jaquet, L. Field, 1952 .