Static Stability Characteristics of a Delta-winged Configuration with a Canard Control and Nacelles at Mach Numbers from 0.25 to 3.50

Static Stability Characteristics of a Delta-winged Configuration with a Canard Control and Nacelles at Mach Numbers from 0.25 to 3.50
Author: LeRoy S. Fletcher
Publisher:
Total Pages: 108
Release: 1962
Genre:
ISBN:

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Static Stability Characteristics of a Delta-winged Configuration with a Canard Control and Nacelles at Mach Numbers from 0.25 to 3.50
Language: en
Pages: 108
NASA Technical Note
Language: en
Pages: 714
Authors:
Categories:
Type: BOOK - Published: 1971 - Publisher:

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Comparison of Several Methods for Estimating Low-speed Stability Derivatives for Two Airplane Configurations
Language: en
Pages: 48
Authors: Herman S. Fletcher
Categories: Airplanes
Type: BOOK - Published: 1971 - Publisher:

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Methods presented in five different publications have been used to estimate the low-speed stability derivatives of two unpowered airplane configurations. One co
Static Stability and Control Characteristics of a Triangular Wing and Canard Configuration at Mach Numbers from 2.58 to 3.53
Language: en
Pages: 62