On the handling qualities of two flying wing aircraft configurations
LMBC Campos, JMG Marques - Aerospace, 2021 - mdpi.com
The coupling of the longitudinal and lateral stability modes of an aeroplane is considered in
two cases:(i) weak coupling, when the changes in the frequency and damping of the …
two cases:(i) weak coupling, when the changes in the frequency and damping of the …
[PDF][PDF] On a Method of Lagrange Multipliers for Cruise Drag Minimization
L Campos, JMG Marques - J. Aerosp. Eng. Mech, 2021 - pdfs.semanticscholar.org
A blended-wing-body is an example of an aircraft configuration with multiple control
surfaces. The most effective use of these control surfaces, eg to minimize cruise drag due to …
surfaces. The most effective use of these control surfaces, eg to minimize cruise drag due to …
On the Extrapolation of Stability Derivatives to Combined Changes in Airspeed and Angles of Attack and Sideslip
LMBC Campos, JMG Marques - Aerospace, 2022 - mdpi.com
The variation in stability derivatives with airspeed and angles of attack and sideslip is
determined using only the dependence of the aerodynamic forces and moments on the …
determined using only the dependence of the aerodynamic forces and moments on the …
On lateral-longitudinal control coupling for short-and long-fuselage BWB aircraft configurations
L Campos, JMG Marques - 2022 - dspace.uevora.pt
The coupling of the longitudinal and lateral stability modes of an aeroplane is considered in
two cases:(i) weak coupling, when the changes in the frequency and damping of the …
two cases:(i) weak coupling, when the changes in the frequency and damping of the …
Design Analysis of a Blended Wing Body
P Das, PR Sharma, RK Parida, A Pradhan… - Recent Advances in …, 2022 - Springer
The goal of this work is to do a thorough state of art study of the Blended Wing Body (BWB)
design and to identify the advantages and limitations of this design. This paper also includes …
design and to identify the advantages and limitations of this design. This paper also includes …
[PDF][PDF] On the Extrapolation of Stability Derivatives to Combined Changes in Airspeed and Angles of Attack and Sideslip. Aerospace 2022, 9, 249
L Campos, JMG Marques - 2022 - academia.edu
The variation in stability derivatives with airspeed and angles of attack and sideslip is
determined using only the dependence of the aerodynamic forces and moments on the …
determined using only the dependence of the aerodynamic forces and moments on the …
Design Analysis of a Blended Wing Body Check for updates Pushpal Das, Prince Roy Sharma, Rama Krishna Parida, Ayush Pradhan
A Nanda, P Chaubdar… - Recent Advances in …, 2022 - books.google.com
A blended wing body, also called as blended body, is a fixed-wing airplane having zero
unmistakable splitting line between the wings & fundamental body of the airplane. With the …
unmistakable splitting line between the wings & fundamental body of the airplane. With the …
[PDF][PDF] On the Handling Qualities of Two Flying Wing Aircraft Configurations. Aerospace 2021, 8, 77
L Campos, JMG Marques - 2021 - academia.edu
The coupling of the longitudinal and lateral stability modes of an aeroplane is considered in
two cases:(i) weak coupling, when the changes in the frequency and damping of the …
two cases:(i) weak coupling, when the changes in the frequency and damping of the …
Optimisation Studies for an Efficient Aerodynamic Configuration of a Blended Wing Unmanned Aerial Vehicle.
MK Padmanabhan, G Santhoshkumar… - … Journal of Vehicle …, 2021 - search.ebscohost.com
There are various configurations and parameters that contribute to the Design of Unmanned
Aerial Vehicles for specific applications. This paper deals with an innovative design of an …
Aerial Vehicles for specific applications. This paper deals with an innovative design of an …