An Investigation of the Lift, Drag, and Static-stability Characteristics of a Triangular-wing Airplane Configuration at Mach Numbers from 3.00 to 6.28
Language: en
Pages: 17

An Investigation of the Lift, Drag, and Static-stability Characteristics of a Triangular-wing Airplane Configuration at Mach Numbers from 3.00 to 6.28

Authors: Hermilo R. Gloria
Categories: Airplanes
Type: BOOK - Published: 1956 - Publisher:

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Lift, drag, and static-stability characteristics of a triangular-wing airplane were determined at Mach numbers from 3.00 to 6.28, angles of attack up to 13 degr
Lift, Drag, and Static Longitudinal Stability Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form
Language: en
Pages: 34

Lift, Drag, and Static Longitudinal Stability Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

Authors: Jim A. Penland
Categories: Airplanes
Type: BOOK - Published: 1955 - Publisher:

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Lift, Drag, and Static Longitudinal Stability Characteristics of Configurations Consisting of Three Triangular Wing Panels and a Body of Equal Length at Mach Numbers from 3.00 to 6.28
Language: en
Pages: 18

Lift, Drag, and Static Longitudinal Stability Characteristics of Configurations Consisting of Three Triangular Wing Panels and a Body of Equal Length at Mach Numbers from 3.00 to 6.28

Authors: Raymond C. Savin
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1956 - Publisher:

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Flight Investigation of the Lift and Drag Characteristics of a Swept-wing, Multijet, Transport-type Airplane
Language: en
Pages: 32

Flight Investigation of the Lift and Drag Characteristics of a Swept-wing, Multijet, Transport-type Airplane

Authors: Ronald Tambor
Categories: Mach number
Type: BOOK - Published: 1960 - Publisher:

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Stability and Drag Characteristics at Mach Numbers from 0.8 to 1.5 of a Free-flight Model Having 3-percent-thick, 60 Degree Triangular Wing and Horizontal Tail Surfaces
Language: en
Pages: 30

Stability and Drag Characteristics at Mach Numbers from 0.8 to 1.5 of a Free-flight Model Having 3-percent-thick, 60 Degree Triangular Wing and Horizontal Tail Surfaces

Authors: Rowe Chapman
Categories: Airplanes
Type: BOOK - Published: 1954 - Publisher:

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A flight test of a rocket-propelled model having 60 degree triangular wing and horizontal tail surfaces 3 percent thick was made to investigate the stability an