BOOKQUE

Transonic Aerodynamic Characteristics of a Model of a Proposed Six-engine Hull-type Seaplane Designed for Supersonic Flight
Dewey E. Wornom
· 1960
Comparison of Longitudinal Aerodynamic Characteristics of Curved and Straight Leading-edge Delta Wings at Mach Numbers 3 and 6
Dewey E. Wornom , Joseph Gera
· 1964
Apollo Saturn 511 Effluent Measurements from the Apollo 16 Launch Operations: An Experiment
Gerald L. Gregory , William C. Hulten , Dewey E. Wornom
· 1974
Transonic Wind-tunnel Investigation of the Effect of Control Span and Large Wing-tip Nacelles on Effectiveness of Spoiler-slot-deflector Controls on an Unswept-wing Fighter-type Airplane
Dewey E. Wornom
· 1960
Transonic Wind-tunnel Investigation of the Interference Between a 45© Sweptback Wing and a Systematic Series of Four Bodies
Donald L. Loving , Dewey E. Wornom
· 1952
Aerodynamic Characteristics of a Flexible-canopy Paraglider Model at a Mach Number of 4.5 for Angles of Attack to 360 ̊and Sideslip Angles from 0 ̊to 90 ̊
Dewey E. Wornom
· 1963
Effluent Monitoring of the December 10, 1974, Titian III-E Launch at Air Force Eastern Test Range, Florida
Dewey E. Wornom , David C. Woods
· 1978
Launch Vehicle Effluent Measurements During the August 20, 1977, Titan III Launch at Air Force Eastern Test Range
David C. Woods
· 1979
No image available
Effects of Body Indentation on the Drag Characteristics of a Delta-wing-body Combination at Transonic Speeds
Dewey E. Wornom
· 1955
No image available
Design and Adaptation of a 2 S.C. Solar Simulator to an Existing Multiwall Ultrahigh Vacuum Chamber
Dewey E. Wornom , F. N. Benning , American Institute of Aeronautics and Astronautics
· 1969