Hypersonic Vehicles

93 books
Special course on aerothermodynamics of hypersonic vehiclesNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Special course on aerothermodynamics of hypersonic vehicles

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1989No page data
Mission and sizing analysis for the Beta II two-stage-to-orbit vehicleShari-Beth Nadell

Mission and sizing analysis for the Beta II two-stage-to-orbit vehicle

Shari-Beth Nadell

1992No page data
Use of tetrafluoromethane to simulate real-gas effects on the hypersonic aerodynamics of blunt vehiclesRobert A Jones

Use of tetrafluoromethane to simulate real-gas effects on the hypersonic aerodynamics of blunt vehicles

Robert A Jones

1978No page data
Hypersonic combined cycle propulsionNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 7h 52m

Hypersonic combined cycle propulsion

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1990472 pp.
The X-33 extended flight test rangeDale A. Mackall
⏱ 11m

The X-33 extended flight test range

Dale A. Mackall

199811 pp.
Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider conceptDavid E. Hahne
⏱ 23m

Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept

David E. Hahne

199723 pp.
Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in helium at Mach 20.3Robert L. Calloway
⏱ 1h 11m

Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in helium at Mach 20.3

Robert L. Calloway

197971 pp.
Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in air at Mach 5.9Robert L. Calloway
⏱ 1h 6m

Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in air at Mach 5.9

Robert L. Calloway

198066 pp.
SRM-assisted trajectory for the GTX reference vehicleJohn Riehl

SRM-assisted trajectory for the GTX reference vehicle

John Riehl

2002No page data
Computation of H2/air reacting flowfields in drag-reduction external combustionH. T. Lai

Computation of H2/air reacting flowfields in drag-reduction external combustion

H. T. Lai

1992No page data
Technical evaluation report on the Fluid Dynamics Panel Symposium on Aerodynamics of Hypersonic Lifting VehiclesSeymour M. Bogdonoff
⏱ 12m

Technical evaluation report on the Fluid Dynamics Panel Symposium on Aerodynamics of Hypersonic Lifting Vehicles

Seymour M. Bogdonoff

198812 pp.
Technical evaluation report on the Fluid Dynamics Panel Symposium on Aerodynamics of Hypersonic Lifting VehiclesS. M. Bodonoff
⏱ 12m

Technical evaluation report on the Fluid Dynamics Panel Symposium on Aerodynamics of Hypersonic Lifting Vehicles

S. M. Bodonoff

198812 pp.
Effect of modifications on aerodynamic characteristics of a single-stage-to-orbit vehicle at Mach 5.9Peter T Bernot
⏱ 30m

Effect of modifications on aerodynamic characteristics of a single-stage-to-orbit vehicle at Mach 5.9

Peter T Bernot

198330 pp.
Development of the X-33 aerodynamic uncertainty modelBrent R. Cobleigh
⏱ 33m

Development of the X-33 aerodynamic uncertainty model

Brent R. Cobleigh

199833 pp.
Comparison between computational and experimental data for a hypersonic laser propelled vehicleD. G. Messitt
⏱ 10m

Comparison between computational and experimental data for a hypersonic laser propelled vehicle

D. G. Messitt

199210 pp.
Evaluation of force measurements of free flying models in a gun tunnelW. Wyborny
⏱ 39m

Evaluation of force measurements of free flying models in a gun tunnel

W. Wyborny

197639 pp.
Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurationsFrank Marconi
⏱ 2h 1m

Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations

Frank Marconi

1976121 pp.
Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in air at Mach 5.9Robert L Calloway
⏱ 1h 6m

Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in air at Mach 5.9

Robert L Calloway

198066 pp.
Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in helium at Mach 20.3Robert L Calloway
⏱ 1h 11m

Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in helium at Mach 20.3

Robert L Calloway

197971 pp.
National Aero-Space PlaneUnited States. General Accounting Office
⏱ 56m

National Aero-Space Plane

United States. General Accounting Office

198856 pp.
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