-
2
-
-
20744441780
-
-
AIAA 2002-0519
-
KOMADINA, S, DRAKE, A, BRUNER, S., "Development of a Quiet Supersonic Aircraft with Technology Applications to Military & Civil Aircraft", AIAA 2002-0519.
-
Development of a Quiet Supersonic Aircraft with Technology Applications to Military & Civil Aircraft
-
-
Komadina, S.1
Drake, A.2
Bruner, S.3
-
5
-
-
0344436102
-
-
AIAA-2002-0771, Reno, NV, Jan
-
SARIC, W.S. & REED, H.L., "Supersonic Laminar Flow Control on Swept Wings", AIAA-2002-0771, Reno, NV, Jan 2002.
-
(2002)
Supersonic Laminar Flow Control on Swept Wings
-
-
Saric, W.S.1
Reed, H.L.2
-
6
-
-
20744459384
-
The potential for a new era of supersonic & hypersonic aviation
-
Strasbourg, Nov.
-
HARRIS. R.V., "The Potential for a New Era of Supersonic & Hypersonic Aviation", Proceedings of European ACTES Symposium, Strasbourg, Nov. 1989.
-
(1989)
Proceedings of European ACTES Symposium
-
-
Harris, R.V.1
-
10
-
-
20744458971
-
Low speed performance optimisation of advanced SCT with different types of LE devices
-
EAC, EAC'94, Toulouse, Oct.
-
NANGIA, R.K., "Low Speed Performance Optimisation of Advanced SCT With Different Types of LE Devices", EAC, Proceedings: "The Supersonic Transport of Second Generation", EAC'94, Toulouse, Oct. 1994.
-
(1994)
Proceedings: "The Supersonic Transport of Second Generation"
-
-
Nangia, R.K.1
-
11
-
-
20744445928
-
Vortex flow dilemmas & control on wing planforms for high speeds
-
Loen, Norway, May
-
NANGIA, R.K. & MILLER, A.S. "Vortex Flow Dilemmas & Control on Wing Planforms for High Speeds", RTO AVT Symposium, Loen, Norway, May 2001.
-
(2001)
RTO AVT Symposium
-
-
Nangia, R.K.1
Miller, A.S.2
-
14
-
-
20744451502
-
-
CEAS European Forum, Bath, UK
-
NANGIA, R. K. & GALPIN, S.A., "Towards Design of High-Lift Krueger Flap Systems with Mach & Reynolds No. Effects for Conventional & Laminar Flow Wings", CEAS European Forum, Bath, UK, 1995.
-
(1995)
Towards Design of High-lift Krueger Flap Systems with Mach & Reynolds No. Effects for Conventional & Laminar Flow Wings
-
-
Nangia, R.K.1
Galpin, S.A.2
-
16
-
-
2942740195
-
Design of conventional & unconventional wings for UAV's
-
"UV for Aerial & Naval Military Operations", Ankara, Turkey, Oct.
-
NANGIA, "Design of Conventional & Unconventional Wings for UAV's", RTA-AVT Symposium, "UV for Aerial & Naval Military Operations", Ankara, Turkey, Oct. 2000.
-
(2000)
RTA-AVT Symposium
-
-
Nangia1
-
17
-
-
20744431984
-
-
AIAA-2002-0709, January
-
NANGIA, R.K., PALMER, M.E. & DOE, R.H., "A Study of Supersonic Aircraft with Thin Wings of Low Sweep", AIAA-2002-0709, January 2002.
-
(2002)
A Study of Supersonic Aircraft with Thin Wings of Low Sweep
-
-
Nangia, R.K.1
Palmer, M.E.2
Doe, R.H.3
-
18
-
-
20744450699
-
-
RTO-AVT-99, Paper 25, Brussels, April
-
NANGIA, R.K., PALMER. M.E., "Unconventional Joined-Wing Concept for Supersonic Aircraft", RTO-AVT-99, Paper 25, Brussels, April 2003.
-
(2003)
Unconventional Joined-wing Concept for Supersonic Aircraft
-
-
Nangia, R.K.1
Palmer, M.E.2
-
20
-
-
2942742089
-
Developing an inverse design method using 3-D membrane analogy
-
NANGIA, R.K., "Developing an Inverse Design Method using 3-D Membrane Analogy", Future Paper.
-
Future Paper
-
-
Nangia, R.K.1
|