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

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
Author: Raymond C. Savin
Publisher:
Total Pages: 18
Release: 1956
Genre: Aerodynamics, Supersonic
ISBN:
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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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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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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 Characteristics of Four Airplane-like Configurations at Mach Numbers from 3.00 to 6.28
Language: en
Pages: 18

Lift, Drag, and Static Longitudinal Stability Characteristics of Four Airplane-like Configurations at Mach Numbers from 3.00 to 6.28

Authors: Stanford E. Neice
Categories:
Type: BOOK - Published: 1955 - Publisher:

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Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds
Language: en
Pages: 80

Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds

Authors: Albert G. Few
Categories: Airplanes
Type: BOOK - Published: 1954 - Publisher:

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The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wing