Amanote Research

Amanote Research

    RegisterSign In

Wing Planform Geometry Effects on Large Subsonic Military Transport Airplanes.

doi 10.21236/ada056124
Full Text
Open PDF
Abstract

Available in full text

Date

February 1, 1978

Authors
Robert M. KulfanJohn D. Vachal
Publisher

Defense Technical Information Center


Related search

Achieving Global Range in Future Subsonic and Supersonic Airplanes

International Journal of Aviation, Aeronautics, and Aerospace
RiskCivilStructural EngineeringReliabilitySafetyQualityAerospace Engineering
2014English

Wing Mass Formula for Subsonic Aircraft

Journal of Aircraft
Aerospace Engineering
1992English

Aircraft System Noise Prediction Uncertainty Quantification for a Hybrid Wing Body Subsonic Transport Concept

2018English

Aerodynamics of High-Subsonic Blended-Wing-Body Configurations

2003English

Case Studies in Aero-Structural Wing Planform and Section Optimization

2004English

Biplane Wing Planform and Flight Performance of the Feathered Dinosaur Microraptor Gui

Proceedings of the National Academy of Sciences of the United States of America
Multidisciplinary
2007English

An Approach to Selecting Gas Turbine Engine Ratings for Fixed Wing Airplanes

1984English

Interference Effects of Very High Bypass Ratio Nacelle Installations on a Low-Wing Transport

1991English

The Effects of Transom Geometry on the Resistance of Large Surface Combatants

1988English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy