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Engineering topics

Driver, C.

Publications and source records attributed to Driver, C..

22 records · Page 2

All sources NASA NTRS DOE OSTI

NASA NTRS1960

Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70 deg delta wing

Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Mach 2.01

DELTA WING↗

NASA NTRS1959

Tabulated data from a pressure-distribution investigation at Mach number 2.01 of the wing of a canard airplane model

Pressure distribution on trapezoidal wing of canard aircraft model in supersonic pressure tunnel - tables

TABLE↗

NASA NTRS1959

STATIC STABILITY AND CONTROL CHARACTERISTICS OF AN AIRPLANE MODEL WITH TAIL SURFACES OUTBOARD OF THE WING TIPS AT A MACH NUMBER OF 2.01

Static stability and control characteristics of aircraft model with tail surfaces outboard of wing tips

SUPERSONIC SPEED↗

NASA NTRS1959

Effect of Forebody Strakes on the Aerodynamic Characteristics in Pitch and Sideslip of a Hypersonic Airplane Configuration at Mach Numbers of 1.41, 2.01, and 6.86

Effect of forebody strakes on aerodynamic characteristics in sideslip and pitch of hypersonic aircraft configurations

PITCH ATTITUDE↗